WO2000022451A2 - A dual channel microwave transmit/receive module for an active aperture of a radar system - Google Patents

A dual channel microwave transmit/receive module for an active aperture of a radar system Download PDF

Info

Publication number
WO2000022451A2
WO2000022451A2 PCT/US1999/021745 US9921745W WO0022451A2 WO 2000022451 A2 WO2000022451 A2 WO 2000022451A2 US 9921745 W US9921745 W US 9921745W WO 0022451 A2 WO0022451 A2 WO 0022451A2
Authority
WO
WIPO (PCT)
Prior art keywords
substrate
power
layers
cavities
channels
Prior art date
Application number
PCT/US1999/021745
Other languages
French (fr)
Other versions
WO2000022451A9 (en
WO2000022451A3 (en
Inventor
John W. Cassen
Stephanie A. Parks
Edward L. Rich, Iii
Gary N. Bonadies
Gary L. Ferrell
John S. Fisher
John W. Gipprich
John D. Gornto
Daniel J. Heffernan
David A. Herlihy
Patrick K. Richard
David W. Strack
Scott K. Suko
George T. Hall
Original Assignee
Northrop Grumman Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Northrop Grumman Corporation filed Critical Northrop Grumman Corporation
Priority to JP2000576296A priority Critical patent/JP2002527971A/en
Priority to AT99968836T priority patent/ATE258313T1/en
Priority to CA002344400A priority patent/CA2344400A1/en
Priority to DE69914354T priority patent/DE69914354T2/en
Priority to AU27052/00A priority patent/AU2705200A/en
Priority to EP99968836A priority patent/EP1125144B1/en
Publication of WO2000022451A2 publication Critical patent/WO2000022451A2/en
Publication of WO2000022451A3 publication Critical patent/WO2000022451A3/en
Publication of WO2000022451A9 publication Critical patent/WO2000022451A9/en

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/03Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/03Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
    • G01S7/032Constructional details for solid-state radar subsystems
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems
    • H01Q21/0025Modular arrays

Definitions

  • This invention relates generally to transmit/receive (T/R) circuit modules utilized, for example, in phased array radar systems and, more particularly, to a dual channel T/R module where two discrete T/R RF signal channels are implemented side-by-side in a common package.
  • T/R transmit/receive
  • Phased array radars utilizing electronically scanned antenna arrays, also referred to as active apertures, require many individually controllable T/R modules which are arranged in an array.
  • the T/R modules are connected to frontally located radiator elements which collectively generate a transmitted radar beam.
  • the beam is normally energized, shaped and directed in azimuth and elevation under electronic control of the signals applied to the individual radiators.
  • a phased array radar system generates successive transmit pulses which are distributed through a transmit manifold and microwave circuitry to the various antenna radiators. Between transmit pulses, the radar system receives and processes successive return signals from the antenna radiators. The return signals are processed through microwave circuitry in the T/R module, collected through a receive manifold, and then processed in the system for target identification.
  • Such a radar system also employs a programmed digital processor to control amplification, attenuation, and phase shifting of transmit and receive signals, thereby determining the amplitude, direction, and shape of the aggregate RF energy beam transmitted by or received by the aperture.
  • Different phase shifts cause different transmit or receive circuit delays in delivery of individual RF radiator signals to control the pattern of RF energy wavefronts associated with the different radiators and which are combined to define the direction and shape of a transmitted or received antenna beam.
  • Each T/R module typically includes a housing structure or package including microwave signal processing means for processing transmitted and received radar signals, control signal processing means interconnected with microwave signal processing components for coupling control signals thereto; and power conditioning means comprising a number of power conditioning components selectively interconnected with the microwave signal processing components and the control signal processing components for providing electrical power thereto. Because such apparatus operates at relatively high power levels, there is also normally provided means for dissipating the heat generated by the various components, particularly the microwave power amplifiers and the power conditioning components associated therewith.
  • T/R modules that are smaller, lighter in weight and lower in cost, while at the same time providing an improvement in operating performance and reliability as well as enhancing ease of installation in an antenna assembly.
  • One known T/R module developed by the assignee of this invention is shown and described in U.S. Patent 4,967,201, entitled, “Multi-Layer Single Substrate Microwave Transmit/Receive Module", granted to Edward L. Rich, III, on October 30, 1990, one of the inventors named in this application.
  • the module disclosed therein is referred to as a "sugar cube" T/R module and includes a single multi-layer substrate having at least two opposed mounting surfaces.
  • the substrate includes a plurality of integrated dielectric layers, electrical conductors and thermal conductors selectively interconnected between the layers of the substrate.
  • Microwave signal processing means is mounted on at least one of the mounting surfaces of the substrate for processing microwave radar signals.
  • Control signal processing means is also mounted on at least one of the mounting surfaces of the substrate for providing control signals for the microwave signal processing means.
  • Power conditioning means is additionally mounted on at least one of the mounting surfaces of the substrate for providing power to power the microwave signal processing means and control signal processing means.
  • a heat sink interface is coupled to a set of thermal conductors or vias passing vertically through the substrate layers and which are positioned in thermal proximity to selected portions of the microwave signal processing means, the power conditioning means, and the control signal processing means for conducting thermal energy away from the heat generating elements mounted on the substrate to a heat sink.
  • the "sugar cube” module comprises a relatively early T/R module design in which basic transmit and receive functions, as then conceived, are embodied in a single modular T/R unit with the operating structure supporting such functions integrated together on a main substrate. While presumably operating as intended, certain inherent deficiencies have been found to exist. For example, while the “sugar cube” module exhibits a compact appearance, it embodies only a single T/R channel and is limited by its design to relatively low RF power output operation and is structurally limited to a single RF connection to an RF manifold. Also, while this type of module has a back-end plug-in capability for certain electrical connections, it has no easy plug-in capability for antenna connections.
  • each module has an antenna radiator built into its front end, thereby creating installation problems in aligning misaligned radiators among installed T/R modules. This is due to the fact that transmitted and received beams require aligned antenna radiators to enable beam control in accordance with system commands.
  • the module-integrated radiator of the "sugar cube” module limits bandwidth during transmission and reception and, because of its simple unpolarized patch structure, restricts radiator operation to a fixed polarization.
  • the "sugar cube" T/R module is thus characterized with polarization inflexibility, whereas good system design requires polarization flexibility to permit variable settings of radiation properties including bandwidth and polarization. For example, if a received signal carries a high noise level in a particular polarization, it is desirable to have the flexibility to control the polarization to an angle where the noise is reduced. In this manner, the signal-to-noise ratio is enhanced and weaker signals can be detected with substantially reduced noise interference.
  • the pin within the single coaxial RF connector between each sugar cube module and the system manifold is susceptible to excessive axial movement in response to antenna mechanical vibrations . Such pin movements can change RF path lengths thereby causing increased noise level and erroneous phase changes which produce beam dispersion and thereby affect intended beam control.
  • problems encountered with the "sugar cube" T/R module is the removal of heat generated by the active components therein. Thermal conductors, coursing vertically through the layered structure of the module to a heat transfer interface provides only limited heat transfer for removal of heat from the active circuit components. As a result, poor thermal performance contributes to a relatively low RF-power-output capability.
  • T/R module More recently, an improved T/R module has been developed by the assignee of this invention and is disclosed in U.S. Patent 5,745,076, entitled “Transmit/Receive Module For Planar Active Apertures", issued to Thomas R. Turlington et al on April 28, 1998.
  • the T/R module disclosed therein and referred to by the assignee as a "StackPak” comprises a module configuration which plugs into the backside of an active aperture and includes discrete RF, DC power and data distribution manifolds which are planar in configuration and are stacked together one on top of the other between a cold plate and an antenna assembly, with the antenna elements and circulators being assembled in a single physical unit which forms the front layer of the aperture.
  • the T/R module itself comprises a multi-chip microwave package comprised of multiple layers of high temperature cofired ceramic (HTCC) including ground planes, stripline, data and DC interconnects, thermal vias and RF inputs/outputs running through the RF assembly for a plurality of monolithic microwave integrated circuit chips (MMICs) which are located in cavities formed in the RF assembly layer.
  • HTCC high temperature cofired ceramic
  • MMICs monolithic microwave integrated circuit chips
  • Each T/R module When “StackPak” T/R modules are installed in place, they are disposed against the cold plate for removal of internally generated heat.
  • Each T/R module moreover, has connector pins extending forwardly from a front module side to make all power, control and RF connections required for the module when it is installed by plugging into the back of the antenna assembly.
  • the forwardly extending pins pass through respective sleeves which, in turn, extend through the stacked layers, thereby enabling the necessary connections to be made between the pins and the antenna radiators, the RF manifolds, and the control and power systems in the various layers.
  • the "StackPak” scheme thus resembles "Swiss cheese” in the sense that the sleeves pass through assembly openings to provide for the necessary DC power, DC digital control, and RF signal connections for the T/R modules.
  • a "StackPak” T/R module can use only a portion of its front surface for the dissipating heat transfer.
  • Gallium arsenide integrated circuits are normally used for RF power amplification in T/R modules, and the temperature and reliability specifications for these devices require increasing heat dissipation for increasing power rating.
  • stackPak T/R modules exhibit relatively poor heat dissipation, and consequently restrict RF power generation, largely because the frontal "real estate" of the T/R module must share heat transfer and electrical connection functions thereby operating with a highly restricted surface area for heat removal.
  • the substrate-based structure of the "StackPak” employs cavities in an RF assembly layer for placement of various RF semiconductor devices to support RF circuitry in a single RF channel, there is no provision for semiconductor device layout or RF circuit routing and RF shielding and isolation between or among two or more discrete T/R channels.
  • the "StackPak" T/R module is also limited by the fact that it employs RF input/output coaxial connectors on three different edges of the module thereby adversely affecting module installation facility, RF circuit length, RF power loss, and RF channel isolation.
  • a low voltage bus normally supplies power to T/R modules from an external power supply, i.e., a DC converter which converts a main source voltage (such as 240V) to a low DC voltage (such as 10V or 11V) for module use.
  • the weight of the low voltage DC (LVDC) bus increases in proportion to the square of the length of the bus path and in proportion to the square of the current carried by the LVDC.
  • Increased RF output power requires increased transmit current pulses, which place increased peaking current demands on the input power supply circuitry, i.e., increased bus path cross-section and weight if increases in bus power losses and heat generation are to be avoided.
  • These principles also apply to any input LVDC path length connected to the external LVDC bus path and extending within the T/R module to power distribution points.
  • the internal LVDC bus path length would normally be relatively short and have less significance to bus power loss and heat generation than the external LVDC bus would have.
  • the LVDC bus structure desirably keeps losses at or below a specified percentage of RF power output as a control on efficiency in producing output RF output power.
  • RF power output increases require significantly increased LVDC bus size and weight.
  • the design of the "StackPak” T/R module substantially affects the RF power output, since excessive bus size and weight is required to reach desirable levels of RF output power. Other factors including poor heat dissipation also limits RF output power in the "StackPak” design.
  • the module can achieve some cost improvement through chip-to-chip wire bonding, but it still carries cost disadvantages resulting from factors including the use of multiple housing/interconnect/seal pieces.
  • T/R modules Notwithstanding the advances made in the art by the above-mentioned T/R modules, there is nevertheless an ongoing need for improvements, which result in reduced weight, cost and size, while at the same time maintaining required performance parameters.
  • T/R modules it is desirable that the following objectives be met: (1) Maximum RF output power; (2) Minimum shielded RF circuitry routing within module; (3) Minimum received noise figure; (4) Maximum isolation between RF channels to facilitate proper beam steering and shaping; (5) Phase adjustability for facilitated beam steering; (6) Minimum heat generation; (7) Minimum thermal resistance allowing maximum heat dissipation; (8) Minimum semiconductor junction temperature rise; (9) Minimum inflow power current; (10) Minimum logic circuit routing; and, (11) Relative ease of installation in an antenna assembly.
  • the prior art in its previous and current states has generally been deficient in meeting the above mentioned objectives individually and collectively.
  • the subject invention is directed to an improved T/R module which meets these objectives while providing reduced cost, greater reliability, and greater maintainability.
  • T/R microwave transmit/receive
  • a T/R module wherein a plurality, preferably two, discrete transmit/receive (T/R) channels are implemented in a single common package and having the capability of providing combined functions, control and power conditioning while utilizing a single multi-cavity, multilayer substrate comprised of high temperature cofired ceramic (HTCC) layers.
  • the ceramic layers have outer surfaces including respective metallization patterns of ground planes and conductors as well as feedthroughs or vertical vias formed therein for providing three dimensional routing of both RF and DC signals so as to configure, among other things, a pair of RF manifold signal couplers which are embedded in the substrate and which transition to an RF interface including a multi-pin RF connector assembly at the front end of the package.
  • a DC and logic interface is located at the rear end of the package and includes means whereby DC power and control signals are connected to a plurality of active circuit components including application specific integrated circuit chips (ASICs) and monolithic microwave integrated circuit chips (MMICs) via spring contact pads.
  • ASICs application specific integrated circuit chips
  • MMICs monolithic microwave integrated circuit chips
  • the MMICs which include RF power amplification circuitry generate most of the heat, are located in multi-level cavities formed in the substrate and are bonded directly to a generally flat heat sink plate which is secured to the bottom of the substrate and acts as an efficient thermal interface to a cold plate type of external heat exchanger.
  • DC power conditioning is also provided by a capacitive bank type of energy storage subassembly externally attached to the rear of the T/R module package for supplying supplementary power for peak power generation.
  • FIG 1 is an electrical block diagram broadly illustrative of a phased array radar system including a T/R module in accordance with the subject invention
  • Figures 2A-2D are perspective top, side and bottom plan views of a T/R module in accordance with the preferred embodiment of the invention
  • FIG 3 is a perspective view of an energy storage capacitor bank located at the rear end of the T/R module shown in Figure 1;
  • Figure 4 is an exploded view of the capacitor bank shown in Figure 3;
  • Figures 5A, 5B, 5C and 5D disclose top, side and bottom plan views and an electrical schematic diagram of the circuit board assembly of the capacitor bank shown in Figure 4;
  • Figure 6 is a top plan view of the interior of the
  • T/R module package shown in Figure 1 and populated with components of each functional sub-system located therein;
  • Figures 7A-7D are side, top, bottom and front plan views of an unpopulated T/R module package shown in Figure
  • FIG. 8 is a cross-sectional view of the T/R module package shown in Figure 7B, taken along the lines 8-8 thereof;
  • FIG. 9 is a cross-sectional view of the T/R module package shown in Figure 7B, taken along the lines 9-9 thereof;
  • FIG 10 is a cross-sectional view of the T/R module package shown in Figure 7B, taken along the lines 10-10 thereof;
  • Figure 11 is an enlarged view of the left side portion of the cross section shown in Figure 8, and being further illustrative of the stack-up of the various HTCC ceramic layers located at the front portion of the T/R module package shown in Figure 7B;
  • Figures 12A-12D are side, top, bottom and front plan views of an unpopulated T/R module package in accordance with the subject invention shown in Figures 7A-7D and now including a bottom heatsink plate attached thereto along with an RF coaxial connector assembly located at the front portion of the package;
  • Figure 13 is a cross-sectional view of the T/R module package shown in Figure 12B, taken along the lines 13-13 thereof;
  • Figure 14 is a diagram further illustrative of the HTCC ceramic layers at the front portion of the package along with patterns of ground and signal vias forming an RF transition between certain layers;
  • Figure 15 is an electrical schematic diagram illustrative of the RF signal paths implemented within the package in accordance with the subject invention.
  • Figure 16 is a simplified electrical block diagram of the dual channel T/R circuit architecture which is implemented with the components shown in Figure 6;
  • Figures 17A-17C are illustrative of the ground metallization pattern, via metallization and top metallization pattern formed in connection with HTCC layer 1 shown in Figure 14;
  • Figures 18A-18B are illustrative of via and top surface metallization pattern formed in connection with HTCC layer 2 shown in Figure 14;
  • Figures 19A-19B are illustrative of the via and top surface metallization pattern formed in connection with HTCC layer 3 shown in Figure 14;
  • Figures 20A-20B are illustrative of the via and a ground metallization pattern formed in connection with HTCC layer 4 shown in Figure 14;
  • Figures 21A-21B are illustrative of the via and top surface metallization pattern formed in connection with HTCC layer 5 of Figure 14;
  • Figures 22A-22B are illustrative of the via and top surface metallization pattern formed in connection with HTCC layer 6 shown in Figure 14;
  • Figures 23A-23B are illustrative of via and ground metallization pattern formed in connection with HTCC layer 7 shown in Figure 14;
  • Figures 24A-24B are illustrative of via and top surface metallization pattern formed in connection with HTCC layer 8 shown in Figure 14;
  • Figures 25A-25B are illustrative of via and top surface metallization pattern formed in connection with HTCC layer 9 shown in Figure 14;
  • Figures 26A-26B are illustrative of via and ground metallization pattern formed in connection with HTCC layer 10 shown in Figure 14. Detailed Description of the Invention
  • FIG. 1 a block diagram broadly illustrative of an active aperture 1 for a radar system 2 including a plurality of phased array antenna elements 3 coupled to a plurality of identical dual channel T/R modules 10 by way of respective RF circulators 4.
  • Each T/R module 10 includes a pair of RF transmit ports TX1 and TX2 and a pair of receive ports RXl and RX2 connected to separate antenna elements 3 and circulators 4 for implementing two separate and distinct T/R channels embodied within one common T/R module 10.
  • Both T/R channels moreover, share a common input port TXM from a transmit manifold 5 and a common output port RXM to a receive manifold 6 which form part of a common RF manifold for the system.
  • the combined output from the receive manifold 6 is fed to the receiver section, not shown, of the radar system 2.
  • RF pulses generated for transmission are fed to the transmit manifold 5 via an array driver 7.
  • the six RF input/output ports TXl, TX2, RXl, RX2, TXM and RXM define an RF interface for the T/R module 10.
  • the module 10 moreover, receives DC power from a DC source 8 and beam steering control signals are received from a beam controller 9 via a power/logic interface. All of these subsystems are under the control of a one or more microprocessors, not shown, located in the radar system 2.
  • the T/R module 10 exhibits an elongated relatively thin profile and implements a pair of discrete transmit/receive channels within a single common package including a multilayer substrate structure 12 comprised of a plurality of high temperature co-fired ceramic (HTCC) layers, to be described hereinafter, bonded together in a generally flat, rectangular configuration including a relatively wide front end portion 14 and a relatively narrow rear portion 16.
  • the substrate 12 acts as a means for interconnecting a number of active and passive components which will be described hereinafter for implementing a dual T/R function for a phased array radar system.
  • a flat metallized rectangular cover 18 fits over a metal ring frame, shown hereinafter, which is bonded to the top of the substrate 12 for protecting the electronic components located within the substrate as well as providing RF shielding therefor.
  • a flat rectangular heat sink plate 20 is also bonded to the bottom of the substrate 12 as shown in Figure 2D and acts as a thermal interface for spreading and transferring heat generated within the module 10 to an external heat exchanger, e.g. cold plate, not shown.
  • RF connectors located in a single connector subassembly 22 which can be easily plugged into the backside of an antenna array and which acts as an RF interface for all RF signals coupled to and from the module 10. These components are, moreover, brazed to the substrate 12 and form a package which is hermetically sealed.
  • All other electrical connections between the module 10 and external apparatus supplying, for example, DC power and control signals, are made through a DC/logic interface located at the other end of the substrate, with the heat sink plate 20 in between, and including a set of twelve (12) spring-like fingers 24 x , 24 2 ...24 ⁇ 2 (Figure 2C) mounted on a small generally rectangular circuit board 26 ( Figures 5A-5C) located on the bottom of the module 10 behind the heat sink plate 20.
  • the circuit board 26 forms part of DC power storage system comprising a capacitive bank subassembly 28 including five (5) electrical capacitors 30 ⁇ , 30 2 ... 30 5 and five (5) fuses 32 : , 32 2 ... 32 5 ( Figure 2A) , respectively connected in series with the capacitors 30 ⁇ ... 30 5 and whose purpose is to supply additional DC power to the module in a well known manner, during peak power operation.
  • the capacitive bank subassembly 28 is further shown in Figures 3, 4, and 5A-5D.
  • the capacitive bank subassembly 28 additionally includes a flat cover member or "comb" 34 affixed to the bottom surface 36 of the circuit board 26 for protecting the fingers 24 ⁇ , 24 2 ...24 ⁇ 2 ( Figure 5C) and a relatively larger top member or "organizer” 38 affixed to the top surface 40 of the circuit board 26 for protecting the capacitors 30 ⁇ ... 30 5 and fuses 32 ⁇ ... 32 5 mounted thereon.
  • the members 34 and 38 are preferably comprised of molded plastic.
  • the "comb" 34 includes an enlarged section 42 at one end which spans the width thereof and includes twelve relatively short identical parallel slots 44 ⁇ , 44 2 , ... 44 i2 which are adapted to fit over and around fingers 24 ⁇ , 24 2 ...24 ⁇ 2 shown in Figures 5B and 5C.
  • the "organizer” 38 includes a raised section 46, as shown in Figure 4, including five open cavities 48 ⁇ ... 48 5 which fit around the capacitors 30 ⁇ ... 30 5 . Behind the cavities 48 ⁇ ... 48 5 are five smaller cavities 50 ⁇ ... 50 5 formed in a relatively thinner portion 52 which surround and protect the fuses 32 ⁇ ... 32 5 .
  • Both the top and bottom surfaces 40 and 36 of the circuit board 26 include patterns of metallization in the form of conductor elements as shown in Figures 5A and 5C for implementing the DC/logic interface.
  • the conductor pattern on the top surface 40 as shown in Figure 5A there are ten equal sized relatively small rectangular conductors 52 ⁇ , 52 2 , ... 52 ⁇ 0 and one double width conductor 54.
  • the conductor element 54 widens out to a larger section of metallization 56 which extends beneath the four larger capacitors 30 2 ... 30 5 .
  • One side of these capacitors are commonly connected to the area of metallization 56.
  • a relatively small rectangular area of metallization 58 extends partially under the front end of the smaller capacitor 30 ⁇ and is connected thereto.
  • capacitors 30 ⁇ "' 30 5 respectively terminate at five like areas of metallization 60 ⁇ , 60 2 ... 60 and connect one side of the capacitors 30 ⁇ ... 30 5 to an adjacent end of the respective fuses 32 ⁇ , • " 32 5 .
  • the opposite end of fuse 32 ⁇ for the smaller capacitor 30 ⁇ connects a small area of metallization 61 which includes a connecting via through the back surface 36 of the board 26.
  • the opposite ends of fuses 32 2 ... 32 5 connect to a common area of metallization 63 which also includes connecting vias to the back surface 36 of the circuit board 26 ( Figure 5C) .
  • the twelve metal spring finger connector elements 24 ⁇ , 24 2 , ... 24 i2 are in registration with the top conductor elements 52 ⁇ , ... 52 ⁇ 0 and 54 and are mutually connected by electrical vias, not shown, through the board 26.
  • Four areas of metallization 62, 64, 66 and 68 are additionally formed on the back surface 36 with the area of metallization 62 being connected to finger connector element 24 3 , the area of metallization 64 being connected to connector element 24 4 , the area of metallization 66 being commonly connected to a first pair of adjacent connector elements 24 5 and 26 6 while the area of metallization 66 is commonly connected to a second pair of connector elements 24 7 , 24 8 .
  • the T/R module 10 operates with two power supply potentials from respective external DC sources, not shown, namely a positive power supply voltage (+10.5VDC) and a negative power supply potential (-6.5VDC).
  • the -6.5 volt negative supply voltage is connected to the module by way of finger element 24 4 and has a ground return by way of finger element 24 3 .
  • Respective connections thereof are made to the upper surface conductor element 52 4 and 52 3 of Figure 5A by vias, not shown, through the board 26.
  • the two areas of metallization 62 and 64 couple across the series connection of the smaller capacitor 30 ⁇ and its associated fuse 32 2 by way of upper surface conductor elements 58 and 61.
  • the positive +10.5 volt supply voltage is commonly connected to connector fingers elements 24 7 and 24 8 where it is then applied to the upper conductor elements 54 and 56, which is common to one side of four parallely connected capacitors 30 2 , 30 3 , 30 4 and 30 5 .
  • a +10.5 volt ground return is provided from fingers 24 5 and 24 6 to the relatively large area of metallization 66 which connects back to conductor element 63 on the front surface 40
  • FIG. 5A This circuit configuration is further shown schematically in Figure 5D.
  • the remaining fingers 24 ⁇ , 24 2 and 24 9 ... 24 ⁇ 2 are utilized for logic input/output signals for the module as shown, for example, comprising the control signals VPROG, BIT, CMD-, CMD+, TR- and TR+ .
  • FIG. 6 is generally illustrative of a structure that is referred to as a TWIN PAK TM because it is populated with two sets of semiconductor integrated circuit chips including, among other things, monolithic microwave integrated circuits (MMICs) and application specific integrated circuits (ASICs) for implementing two separate and independent T/R channels. While two T/R channels are contemplated for the preferred embodiment of this invention, it is conceivable that more than two channels could be implemented, if need be, with a more innovative design.
  • MMICs monolithic microwave integrated circuits
  • ASICs application specific integrated circuits
  • each of the two channels of the subject invention respectively include: a module controller 70, 72; a switch/phase shifter 74, 76; a pre or post amp/attenuator/switch/driver amplifier 78, 80; a low noise amplifier 82, 84; a receiver protector 86 and 88 and a power amplifier 90 and 92.
  • a shared gate regulator 94 Located between these elements are a shared gate regulator 94, a POWERFET switch 96, and power controller 98.
  • the substrate 12 as further shown in Figures 7B and 12B, includes six multi-level cavities, three of which, as shown by reference numerals 100, 102 and 104, are located along one side edge of the substrate 12 and are used in connection with one of the T/R channels, while the other three cavities 106, 108 and 110 comprise like multi-level cavities along the other side edge of the substrate 12 and used in connection with the other T/R channel.
  • the cavities 100 ... 110 are, moreover, shown in the sectional views 8, 9, 10 and 13.
  • the other cavities 100, 102 and 106, 108 include two or more integrated circuit components therein as shown in Figure 6.
  • Such an arrangement results in separate isolated cavities for the RF gain stages in the input and output of the transmit circuitry.
  • the two rear cavities 100 and 106 share respective switch/phase shifter MMICs 74, 76 and post-amp/attenuator/switch/driver amplifiers MMICs 78, 80.
  • the intermediate cavities 102 and 108 respectively include low noise amplifiers (LNA) 82, 84 and receiver protectors 86, 88.
  • LNA low noise amplifiers
  • module controllers 70 and 72 do not reside in cavities, but are located on a top HTCC layer of the substrate 12.
  • the two module controllers 70 and 72, the gate regulator 94 and power controller 98 are comprised of ASICs, while the phase shifter/switches 74, 76; the post amplifier/attenuator/switch/driver elements 78, 80; the low noise amplifiers 82, 84, and the two output power amplifiers 90, 92 comprise MMICs which reside in the cavities 100, 102, 104, 106, 108 and 110, and which are placed in direct contact with and bonded to the heat sink plate 20 as shown, for example, in Figure 14.
  • heat sink plate 20 is preferably comprised of a copper tungsten alloy to enhance heat dissipation of the heat generated by the MMICs through the plate 20 to an external heat exchanger, not shown, other heat conducting metallic materials can also be used when desired, such as copper molybdenum or aluminum silicon carbide.
  • a metal ring frame as shown by reference numeral 112 is brazed on the top of the substrate 12 as shown, for example, in Figures 6 and 13 and is configured to border a major portion of the substrate 12 behind the front end portion 14 so as to encircle the six cavities 100, 102 ... 110 as well as the regions including the module controllers 70 and 72 and the shared circuit components 94, 96 and 98 residing in the center of the substrate on either side of the T/R channels. Its purpose is to receive and support the flat cover member 18 shown in Figures 1 and 2A and provide isolation and RF shielding from respective elements.
  • Figures 7A-7D are intended to illustrate the construction of the substrate 12 in its unpopulated state, and without an RF connector 22 assembly and heat sink plate 20.
  • Figures 12A-12D are intended to show the same unpopulated structure of the substrate 12, but now also including the heat sink plate 20 and the RF connector assembly 22.
  • the stippling is intended to denote surfaces which include areas of exposed metallization, e.g. gold.
  • Figure 7C is illustrative of the exposed bottom surface 114 of the substrate 12 and includes openings therein 116, 118 ... 126 and which correspond to the shape of the cavities 100, 102 ... 110 shown in Figure 7B looking from the top.
  • the surface 114 comprises the lowermost surface of the lowermost layer 13 ⁇ of a plurality of stacked HTCC layers 13 : ... 13 ⁇ 5 shown in Figures 8-11, 13 and 14.
  • the metallization pattern comprises a ground plane of metallization 128 including the two input conductor segments 55 3 and 55 5 and the isolated input/output conductor segments 55 ⁇ , 55 2/ 55 4 , 55 6 ... 55 ⁇ 0 which mate with the conductor segments 52 ⁇ "" 52 ⁇ , 54, 52 7 ... 52 ⁇ o of the capacitor bank connector plate 26 as shown, for example, in Figure 5A. It can be seen that conductor segment 55 3 of Figure 7C and segment 52 3 of Figure 5A form a common ground connection along with segment 55 5 of Figure 7C and segments 52 5 , 52 6 of Figure 5A.
  • Figure 7D shows the face 130 of the front end portion 14 of the substrate 12 including six (6) isolated circular segments of metallization 132 ⁇ , 132 2 ... 132 6 which define the pin location of six (6) aligned blind mate press on connectors 134 ⁇ , 134 2 ... 134 6 _ included in the connector assembly 22, as further shown in Figure 12D, and enclosed in an elongated generally rectangular shroud 136.
  • the connector assembly 22 results in an in-line connector assembly including two separate transmit (Tx) connectors 134 2 and 134 6 , two separate receive (Rx) connectors 134 ⁇ and 134 5 for individual connection to antenna elements of an array, but only two manifold connectors 134 3 and 134 4 which share connection to a transmit and receive manifold and which allows the module 10 to be easily plugged into the array during assembly and thereafter removed when required.
  • Tx transmit
  • Rx receive
  • the inner surface of the heat sink plate 20 also includes metallization which covers the cavity openings 116, 118 ... 126 of Figure 7C. It is this surface on which all of the heat generating MMICs located in the six cavities 100, 102 ... 110 are mounted.
  • the substrate 12 is comprised of fifteen contiguous layers 13] . , 13 2 ... 13i5 of HTTC material, ranging in thickness between .006 in. to .020 in. and wherein layers 13 ⁇ through 13 10 are used to form the six cavities 100, 102, 104, 106, 108 and 110.
  • HTCC high temperature co-fired ceramic
  • the multi-level structure of the substrate 12 as shown in Figure 14 permit passive components to be located within the cavities on layer or steps 13 4 , for example, and for implementing wire bond connections between chips at layer 13 2 and for providing connections to the MMICs located on the heat sink plate 20.
  • reference numeral 90 represents the RF power output amplifier MMIC 90 located in cavity 104.
  • the layer 13 ⁇ 0 comprises a layer upon which the power controller ASIC 98 is located.
  • layer 13 ⁇ 0 is the layer upon which the ring frame 112 member ( Figure 13) and connector pins 138 ⁇ ... 138 6 of a blind mate press-on connector assembly 22 are brazed.
  • the connector pins 138 ⁇ "' 138 6 comprise elements which are manufactured and supplied by Gilbert Engineering, Inc.
  • the five uppermost layers 13 u " ' 13 ⁇ 5 shown at the right on Figure 14, comprise what is referred to as "dummy" layers and form the forward portion 14 of the substrate 12.
  • the substrate layers 13 ⁇ ... 13 ⁇ 0 provide the ability to implement 3-D routing of both RF signals and DC signals within the substrate 12 as well as embedding a pair of RF manifold couplers therein.
  • RF routing and transitions comprise coupling the inputs and outputs from the six pin connector assembly 22 and implementing a well matched structure up to all the MMICs located in the cavities 100 ... 110.
  • Shielded 3-D routing is implemented within the substrate 12 and results from the layers 13 ⁇ '" 13 ⁇ o being comprised of contiguous discrete dielectric layers, each with its own pattern of ground plane and vertical feed- throughs or vias, along with respective stripline conductor patterns formed on the top surface thereof as will be shown hereinafter.
  • RF signals enter and leave the module 10 by means of the connector assembly 22.
  • Connector assembly 22 includes six like RF coaxial connectors 134 ⁇ ... 134 6 , including pins 138 ⁇ ... 138 6 , arranged in linearly ( Figure 12D) within and across the shroud member 136.
  • the connector pin 138i is shown connected to a stripline conductor 140 on the top of the HTCC layer 13 10 .
  • Stripline conductor 140 extends inwardly where it connects to a vertical via 142 which descends to a length of stripline conductor 144 on the top of layer 13 6 .
  • a length of stripline conductor 146 which extends under conductor 144.
  • stripline conductor 146 connects to a vertical via 148 which descends to the top of layer 13 2 and stripline conductor 150.
  • a bond wire member 151 which connects the MMIC 90.
  • a stripline conductor element 149 which acts as a capacitive stub is also shown located on the top of layer 13 ⁇ directly beneath the bond wire connection of member 151 to conductor 150.
  • Isolation and shielding for the RF coupler configured by stripline conductors 144 and 146 are further provided by upper and lower ground planes 152 and 154 including multiple vertical vias 156, 158 and 162 terminating the top of layers 13 4 and 13 7 , respectively.
  • the shroud 136 is coupled to three ground planes 164, 166 and 168 which are further interconnected by multiple vertical vias 170, 172 and 174.
  • This in combination with the metal alloy plate 20, provides shielding for the signals passing to and from the RF connector assembly 22. Achieved thereby is an RF structure including a connector to stripline section, a stripline to stripline section, a coupler section and a stripline to MMIC section.
  • Minimal RF output routing is obtained by the configuration of the invention shown in Figure 14.
  • the benefit obtained results from the fact that about 1 to 2 dB of losses can be produced by each inch of RF routing from a power amplifier to the RF interface through one or more module layers. Such a loss would drop the output RF power from 100% nominal to about 80% with use of alumina ceramic dielectric as substrate and layer material, or to about 63% with use of common black ceramic.
  • FIG. 17A, 17B and 17C depicted thereat is the lowermost layer 13 ⁇ of the substrate 12 and one which includes a ground plane 128 (Figure 7C) , the face-up side of which is shown in Figure 17A along with the DC logic conductor interface elements 55 ⁇ ... 55 ⁇ 0 .
  • Figure 7C ground plane 128
  • Generally rectangular unmetallized areas 116 ... 126 which define openings for the six cavities 100, 102 ... 110 are also shown in Figure 17A. This same pattern of openings also exists in the upper HTTC layers 13 2 ... 13 ⁇ 0 .
  • Figure 17B discloses the pattern of vias fabricated vertically through HTCC layer 13 ⁇ .
  • the circular via patterns 180, 182, 184 ... 198, 200 are illustrative of a plurality of cylindrical vertical via patterns which can be seen in combination with the upper ceramic layers 13 2 and 13 3 such as Figures 18A and 19B to form cylinder-like shielded conduits for RF signal carrying vias centralized in the circular patterns of vias and transitioning vertically between layers.
  • Pairs of mutually parallel lines of vias 202, 204 ... 216, 218 represent shielding type passageways for signal carrying stripline conductors located in layer 13 2 ( Figures 18A, 18B) above layer 13 ⁇ .
  • the top surface of layer 13 ⁇ as shown in Figure 17C includes a stripline metallization pattern which acts in concert with the underlying lines of vias 202 ... 218 to form a bottom channelized RF shielding layer for the signal carrying conductors located above on layer 13 2 along with stripline elements 222, 224 ... 236, 238.
  • the arrangement of vertical vias shown in Figure 18A is substantially the same as that shown in Figure 17A, with the exception of an absence of vias at the area of reference numeral 240.
  • the pattern of metallization of Figure 18B matches that of Figure 17C, but now also includes, for example, RF signal carrying stripline conductors 240, 242 ...
  • FIG. 19A With respect to the third layer 13 3 shown in Figures 19A and 19B, its pattern of vertical vias as shown in Figure 19A also matches the via patterns of Figures 17B and 18A, particularly with respect to the parallel line pairs of vias 202 ... 218.
  • the top surface of metallization of Figure 19B includes substantially the same stripline pattern shown in Figure 17C but with an extra area of metallization 281 and thus acts as a top channelized shielding layer thereby implementing a shielded outer conductor or conduit for the signal carrying conductors located in layer 13 2 "
  • the bottom three layers 13 ⁇ , 13 2 , and 13 3 of HTCC material thus implement one of two levels of RF routing and one for routing RF signals between the various MMICs in the cavities 100 ... 110 and the connector assembly 22 ( Figures 12D)
  • layer 13 4 as shown in Figures 20A and 20B comprises an HTCC layer implementing a first internal ground plane. Its pattern of vias, as shown in Figure 20A, substantially matches the via pattern shown in the underlying layer 13 3 ( Figure 19A) .
  • the upper surface of layer 13 4 ( Figure 20B) comprises a ground plane of stripline as shown by reference numeral 282, along with a plurality of circular openings within which are located vias 241, 243 ... 267, as shown. These vias match the underlying like numbered vias in Figure 19B.
  • the intermediate layers 13 5 , 13 6 and 13 7 in addition to including specific patterns of conductors and vias, also implement a pair of RF signal couplers which connect to both T/R channels and which results in eliminating two relatively expensive GPPO manifold connectors.
  • An example of how such a coupler is fabricated in the subject invention is shown in Figure 14 with reference to the stripline conductors shown by reference numerals 144 and 146.
  • FIG. 21A shown in Figure 21A is a vertical via pattern of vias and stripline which also includes, inter alia, the circular via patterns 180, 181, 182 ... 198, 200, but also now includes new parallel line pairs of vias 284, 286, 288, and 290, with pairs 286, 288 and 290 terminating in respective additionally circular via patterns 292, 294 and 296 located at the RF connector end of the substrate.
  • shielding striplines 304, 306 ... 312, 314 are again formed around the openings for the cavities 102, 104 ... 110.
  • receive manifold coupler segment 322 connects to conductor 336 and via 184 while the opposite side thereof connects to an elongated conductor 338 which passes through conductor pair 300 to a vertical via 340 in circular via pattern 292 and which then connects to RF connector 134 3 in Figure 12D.
  • Figure 21B also depicts a shield conductor pair 341 which mutually shares a conductor with adjacent shield conductor pair 302.
  • a vertical via 342 is also now provided in circular via pattern 296.
  • the via pattern of layer 13 ⁇ illustrated in Figure 22A is similar to that in the underlying layer 13 5 shown in Figure 21A.
  • the stripline conductor patterns on the top surface of the layer 13 6 again operate as shielding elements for implementing shielding enclosures for the underlying RF conductors 300 and 330 shown in Figure 2IB as well as an RF conductor line 344 connected between via 179 and one side of transmit manifold coupler segment 324.
  • an RF conductor line 346 for the received signal (RX2) of the second T/R channel is connected between via 265 and vertical via 342 in circular via pattern 296 at the RF connector end of the substrate 12.
  • one side of receive manifold coupler segment 322 connects to conductor 348 and via 257 while the other side connects to conductor 350 and via 263.
  • layers 13 5 and 13 6 which overlay the ground plane metallization 282 of layer 13 4 as shown in Figure 20B comprise a second level of RF routing which is primarily used for routing RF signals to and from the manifold couplers 320 and 322; however, as noted above, layer 13 6 also routs the RF receive signal from the antenna array and connector assembly 22 ( Figure 12D) to the low noise amplifier 84 located in cavity 108.
  • Layer 13 7 comprises a second ground plane layer. It includes a via pattern as shown in Figure 23A which substantially matches the via pattern in the underlying layer 13 6 shown in Figure 22A.
  • Figure 23B is illustrative of the metallization pattern formed on the top of layer 13 7 and comprises a ground plane metallization 352 but now includes six (6) circular openings for the six vertical RF connector vias 251, 255, 267, 334, 340 and 342.
  • the ground plane metallization 352 also includes seven (7) isolation stubs 354, 356, ... 364, 366 which are located between the six(6) RF connectors 134 ⁇ ... 134 6 ( Figure 12D) .
  • the upper HTCC layers 13 8 , 13 9 and 13 ⁇ o provide a level of routing of DC power and logic control signals between the various MMICs and ASICs as well as providing for connection of the pins 138 ⁇ , 138 2 ... 138 6 of the RF connectors 134 ⁇ , 134 2 , ... 134 6 of the RF connector assembly 22 at the front portion 14 of the substrate 12.
  • the pattern of vertical vias as shown in Figs. 24A and 25A are similar but now include six (6) arcuate via patterns 368, 370 ... 376, 378 forward of the vias 251 ... 267 at the connector end of the substrate.
  • the top surfaces thereof have selectively different patterns of stripline conductor metallization as shown in Figs 24B and 25B.
  • the upper surface of metallization of layer 13 8 as shown in Figure 24B includes a conductor pattern of stripline conductors, isolation borders, as well as seven (7) connector pin isolation stubs 380 ... 402 which match the stubs 354 ... 366 of layer 13 7 ( Figure 23B) .
  • the via pattern for layer 13 10 as shown in Figure 26A is similar to the via pattern shown in Figure 25A for the underlying layer 13 9 ; however, in addition to the arcuate via patterns 368 ... 378 included therein are vias 404 ... 414 aligned with vias 251 ... 267 and which are provided for mating with six stripline conductor elements 416 ... 426 as shown in Figure 26B.
  • the six connector pins 138 ⁇ , 138 2 ... 138 6 are brazed to the stripline conductor elements 416 ... 426 in the fabrication of the substrate 12.
  • a set of seven (7) pin isolation stubs 430 ... 442 as shown in Figure 26B are located between and insulated from the pin connector strips 416 ... 426.
  • a ground plane is further provided by a large metallization area shown by reference numeral 444, including openings formed therein for accommodating the MMICs and ASICs located in the cavities 100 ... 110 of the substrate 12.
  • the RF signal paths implemented thereby are shown in the block diagram of Figure 15.
  • RF signals for two discrete T/R channels are coupled to and from the substrate 12 via connector assembly 22 located at one end of the substrate. DC power and logic control signals are applied to the substrate 12 at the other end as shown.
  • the RF signal paths depicted in Figure 15 can be found on the top surface of layer 13 2 as shown in Figure 18B and the top surfaces of layers 13 5 and 13 6 as shown in Figures 21B and 22B, respectively, and where, as noted before, RF routing is broken into two sections, a lower section including layers 13 ⁇ , 13 2 , and 13 3 and an upper section including layers 13 5 and 13 6 .
  • Layer 13 2 of the bottom RF section is used primarily for routing RF signals between MMICs and to/from the connector assembly 22, while layers 13 5 and 13 6 of upper section are used for the implementation of the two manifold couplers 320 and 322.
  • layer 13 6 is also used for routing the RF received signal for one of the channels.
  • each channel operates independently of the other, while sharing in a unique manner not only the transmit and receive manifolds by way of the RF couplers 320 and 322, but also the power and operation of the gate regulator 94, the POWERFET switch 96, and the power controller 98.
  • each channel includes: a receiver protector (R/P) element 86, 88; a low noise amplifier 82, 84 including two stages of amplification; an RF switch and phase shifter (SW/PHS) 74, 76 including a single pole double throw RF switch and a digitally controlled phase shifter; an amplifier/gain trim attenuator/switch/driver amp (AMP/ATTN/SW/DVR) 78, 80 including three stages of pre amp or post amp amplification, a second single pole, double-throw switch located between a pair of digitally controlled gain trim attenuators and two stages of driver amplification; and a power amplifier 90, 92 including three stages of RF power amplification.
  • R/P receiver protector
  • SW/PHS RF switch and phase shifter
  • AMP/ATTN/SW/DVR amplifier/gain trim attenuator/switch/driver amp
  • Beam control signals are fed from the beam steering controller 9 ( Figure 1) to separate module controllers 70 and 72 so as to respectively provide phase and amplitude control over RF transmit and receive signals in the respective T/R channels.
  • the module controllers 70 and 72 preferably operate on a limited basis of shared module control via the power controller 98 by providing crossover channel control so that in the event one of the module controllers fails, the other module controller takes over. Further, either module controller 70 or 72 will shut down the entire module 10 upon the detection of certain conditions, in order to prevent faulty module operation from adversely affecting the accuracy of overall beam control.
  • a multi-layer substrate which may be implemented as an MLCC such as an HTCC structure provides a number of attendant advantages in terms of design flexibility, performance and at lower cost.
  • the multi- layer nature of the structure permits isolated crossovers of both RF and DC, due to the fact that ground planes are located between signal lines.
  • the overall density of the assembly is increased due to both the ability to integrate certain passive microwave components, and the ability to perform 3-D routing of both RF and DC signals.
  • the T/R modules 10 can be structured for ease of module assembly and ease of assembly of the module into the antenna array.
  • the invention further enables performance and cost improvements to be realized in a multi-channel T/R module which can be conveniently plugged into an antenna assembly while making electrical and heat sink connections simultaneously between the module and the assembly.
  • RF connections are made with high stability against vibration, thereby supporting quality RF signal processing, and the heat sink connection is made with large surface contact area, thereby supporting higher heat dissipation, reduced rise in junction temperatures of module semiconductor devices, and higher module RF power capability.

Abstract

Two transmit/receive (T/R) channels are implemented in a single T/R module providing combined functions, control and power conditioning while utilizing a single multicavity, multilayer substrate comprised of high temperature cofired ceramic (HTCC) layers. The ceramic layers have outer surfaces for providing three dimensional routing of both shielded RF and DC power and logic control signals. Monolithic microwave integrated circuits, attached to DC power and logic control signals, are located in multilevel cavities formed in the substrate and bonded directly to a heat sink plate, secured to the bottom of the substrate. DC power conditioning is provided by a capacitive bank supplying supplementary power to the module during peak power operation. The T/R module is one module of an array of like T/R modules coupled to an active aperture of a radar system.

Description

A DUAL CHANNEL MICROWAVE TRANSMIT/RECEIVE MODULE FOR AN ACTIVE APERTURE OF A RADAR SYSTEM
Background of the Invention Cross Reference To Related Applications
This application is related to U.S. Serial No. 09/158,832 (Northrop Grumman Docket No. BD-98-112) entitled, "Transmit/Receive Module Having Multiple Transmit/Receive Paths With Shared Circuitry", filed in the names of John W. Cassen et al on September 23, 1998; and
U.S. Serial No. 09/158,827 (Northrop Grumman Docket No. BD-98-111) entitled "Antenna Assembly Including Dual Channel Microwave Transmit/Receive Modules ", filed in the names of John W. Cassen et al on September 23, 1998.
Both of these applications are assigned to the assignee of this invention and, moreover, are intended to be incorporated herein by reference.
Field of the Invention
This invention relates generally to transmit/receive (T/R) circuit modules utilized, for example, in phased array radar systems and, more particularly, to a dual channel T/R module where two discrete T/R RF signal channels are implemented side-by-side in a common package. Description of Related Art Phased array radars utilizing electronically scanned antenna arrays, also referred to as active apertures, require many individually controllable T/R modules which are arranged in an array. The T/R modules are connected to frontally located radiator elements which collectively generate a transmitted radar beam. The beam is normally energized, shaped and directed in azimuth and elevation under electronic control of the signals applied to the individual radiators.
A phased array radar system generates successive transmit pulses which are distributed through a transmit manifold and microwave circuitry to the various antenna radiators. Between transmit pulses, the radar system receives and processes successive return signals from the antenna radiators. The return signals are processed through microwave circuitry in the T/R module, collected through a receive manifold, and then processed in the system for target identification.
Such a radar system also employs a programmed digital processor to control amplification, attenuation, and phase shifting of transmit and receive signals, thereby determining the amplitude, direction, and shape of the aggregate RF energy beam transmitted by or received by the aperture. Different phase shifts cause different transmit or receive circuit delays in delivery of individual RF radiator signals to control the pattern of RF energy wavefronts associated with the different radiators and which are combined to define the direction and shape of a transmitted or received antenna beam.
Each T/R module according to the known prior art typically includes a housing structure or package including microwave signal processing means for processing transmitted and received radar signals, control signal processing means interconnected with microwave signal processing components for coupling control signals thereto; and power conditioning means comprising a number of power conditioning components selectively interconnected with the microwave signal processing components and the control signal processing components for providing electrical power thereto. Because such apparatus operates at relatively high power levels, there is also normally provided means for dissipating the heat generated by the various components, particularly the microwave power amplifiers and the power conditioning components associated therewith.
Accordingly, there is an ongoing development in this field of microwave technology to produce T/R modules that are smaller, lighter in weight and lower in cost, while at the same time providing an improvement in operating performance and reliability as well as enhancing ease of installation in an antenna assembly. One known T/R module developed by the assignee of this invention is shown and described in U.S. Patent 4,967,201, entitled, "Multi-Layer Single Substrate Microwave Transmit/Receive Module", granted to Edward L. Rich, III, on October 30, 1990, one of the inventors named in this application. The module disclosed therein is referred to as a "sugar cube" T/R module and includes a single multi-layer substrate having at least two opposed mounting surfaces. The substrate includes a plurality of integrated dielectric layers, electrical conductors and thermal conductors selectively interconnected between the layers of the substrate. Microwave signal processing means is mounted on at least one of the mounting surfaces of the substrate for processing microwave radar signals. Control signal processing means is also mounted on at least one of the mounting surfaces of the substrate for providing control signals for the microwave signal processing means. Power conditioning means is additionally mounted on at least one of the mounting surfaces of the substrate for providing power to power the microwave signal processing means and control signal processing means. A heat sink interface is coupled to a set of thermal conductors or vias passing vertically through the substrate layers and which are positioned in thermal proximity to selected portions of the microwave signal processing means, the power conditioning means, and the control signal processing means for conducting thermal energy away from the heat generating elements mounted on the substrate to a heat sink.
The "sugar cube" module comprises a relatively early T/R module design in which basic transmit and receive functions, as then conceived, are embodied in a single modular T/R unit with the operating structure supporting such functions integrated together on a main substrate. While presumably operating as intended, certain inherent deficiencies have been found to exist. For example, while the "sugar cube" module exhibits a compact appearance, it embodies only a single T/R channel and is limited by its design to relatively low RF power output operation and is structurally limited to a single RF connection to an RF manifold. Also, while this type of module has a back-end plug-in capability for certain electrical connections, it has no easy plug-in capability for antenna connections. Instead, each module has an antenna radiator built into its front end, thereby creating installation problems in aligning misaligned radiators among installed T/R modules. This is due to the fact that transmitted and received beams require aligned antenna radiators to enable beam control in accordance with system commands.
Moreover, the module-integrated radiator of the "sugar cube" module limits bandwidth during transmission and reception and, because of its simple unpolarized patch structure, restricts radiator operation to a fixed polarization. The "sugar cube" T/R module is thus characterized with polarization inflexibility, whereas good system design requires polarization flexibility to permit variable settings of radiation properties including bandwidth and polarization. For example, if a received signal carries a high noise level in a particular polarization, it is desirable to have the flexibility to control the polarization to an angle where the noise is reduced. In this manner, the signal-to-noise ratio is enhanced and weaker signals can be detected with substantially reduced noise interference.
Further, in an antenna assembly employing "sugar cube" T/R modules, the pin within the single coaxial RF connector between each sugar cube module and the system manifold is susceptible to excessive axial movement in response to antenna mechanical vibrations . Such pin movements can change RF path lengths thereby causing increased noise level and erroneous phase changes which produce beam dispersion and thereby affect intended beam control. Among other problems encountered with the "sugar cube" T/R module is the removal of heat generated by the active components therein. Thermal conductors, coursing vertically through the layered structure of the module to a heat transfer interface provides only limited heat transfer for removal of heat from the active circuit components. As a result, poor thermal performance contributes to a relatively low RF-power-output capability.
More recently, an improved T/R module has been developed by the assignee of this invention and is disclosed in U.S. Patent 5,745,076, entitled "Transmit/Receive Module For Planar Active Apertures", issued to Thomas R. Turlington et al on April 28, 1998. The T/R module disclosed therein and referred to by the assignee as a "StackPak" comprises a module configuration which plugs into the backside of an active aperture and includes discrete RF, DC power and data distribution manifolds which are planar in configuration and are stacked together one on top of the other between a cold plate and an antenna assembly, with the antenna elements and circulators being assembled in a single physical unit which forms the front layer of the aperture.
The T/R module itself comprises a multi-chip microwave package comprised of multiple layers of high temperature cofired ceramic (HTCC) including ground planes, stripline, data and DC interconnects, thermal vias and RF inputs/outputs running through the RF assembly for a plurality of monolithic microwave integrated circuit chips (MMICs) which are located in cavities formed in the RF assembly layer. The module's architecture includes a single transmit/receive RF signal channel that shares its control functions of gain trim, phase shift and intermediate power amplification in both the transmit and receive modes of operation.
When "StackPak" T/R modules are installed in place, they are disposed against the cold plate for removal of internally generated heat. Each T/R module, moreover, has connector pins extending forwardly from a front module side to make all power, control and RF connections required for the module when it is installed by plugging into the back of the antenna assembly. The forwardly extending pins pass through respective sleeves which, in turn, extend through the stacked layers, thereby enabling the necessary connections to be made between the pins and the antenna radiators, the RF manifolds, and the control and power systems in the various layers.
The "StackPak" scheme thus resembles "Swiss cheese" in the sense that the sleeves pass through assembly openings to provide for the necessary DC power, DC digital control, and RF signal connections for the T/R modules. In dissipating heat to a heat exchanger, a "StackPak" T/R module can use only a portion of its front surface for the dissipating heat transfer. Gallium arsenide integrated circuits are normally used for RF power amplification in T/R modules, and the temperature and reliability specifications for these devices require increasing heat dissipation for increasing power rating. Thus, "StackPak" T/R modules exhibit relatively poor heat dissipation, and consequently restrict RF power generation, largely because the frontal "real estate" of the T/R module must share heat transfer and electrical connection functions thereby operating with a highly restricted surface area for heat removal.
While the substrate-based structure of the "StackPak" employs cavities in an RF assembly layer for placement of various RF semiconductor devices to support RF circuitry in a single RF channel, there is no provision for semiconductor device layout or RF circuit routing and RF shielding and isolation between or among two or more discrete T/R channels.
The "StackPak" T/R module is also limited by the fact that it employs RF input/output coaxial connectors on three different edges of the module thereby adversely affecting module installation facility, RF circuit length, RF power loss, and RF channel isolation.
The "StackPak" T/R module is furthermore hindered by limited capacity for interfacing DC power from an external power supply to the T/R module. Thus, in an active aperture, a low voltage bus normally supplies power to T/R modules from an external power supply, i.e., a DC converter which converts a main source voltage (such as 240V) to a low DC voltage (such as 10V or 11V) for module use. The weight of the low voltage DC (LVDC) bus increases in proportion to the square of the length of the bus path and in proportion to the square of the current carried by the LVDC. Increased RF output power requires increased transmit current pulses, which place increased peaking current demands on the input power supply circuitry, i.e., increased bus path cross-section and weight if increases in bus power losses and heat generation are to be avoided. These principles also apply to any input LVDC path length connected to the external LVDC bus path and extending within the T/R module to power distribution points. However, the internal LVDC bus path length would normally be relatively short and have less significance to bus power loss and heat generation than the external LVDC bus would have. In accordance with good design practice, the LVDC bus structure desirably keeps losses at or below a specified percentage of RF power output as a control on efficiency in producing output RF output power. Thus, RF power output increases require significantly increased LVDC bus size and weight.
Thus, the design of the "StackPak" T/R module substantially affects the RF power output, since excessive bus size and weight is required to reach desirable levels of RF output power. Other factors including poor heat dissipation also limits RF output power in the "StackPak" design. Although the module can achieve some cost improvement through chip-to-chip wire bonding, but it still carries cost disadvantages resulting from factors including the use of multiple housing/interconnect/seal pieces.
Notwithstanding the advances made in the art by the above-mentioned T/R modules, there is nevertheless an ongoing need for improvements, which result in reduced weight, cost and size, while at the same time maintaining required performance parameters. In achieving further development of T/R modules, it is desirable that the following objectives be met: (1) Maximum RF output power; (2) Minimum shielded RF circuitry routing within module; (3) Minimum received noise figure; (4) Maximum isolation between RF channels to facilitate proper beam steering and shaping; (5) Phase adjustability for facilitated beam steering; (6) Minimum heat generation; (7) Minimum thermal resistance allowing maximum heat dissipation; (8) Minimum semiconductor junction temperature rise; (9) Minimum inflow power current; (10) Minimum logic circuit routing; and, (11) Relative ease of installation in an antenna assembly.
In summary, the prior art in its previous and current states has generally been deficient in meeting the above mentioned objectives individually and collectively. The subject invention, therefore, is directed to an improved T/R module which meets these objectives while providing reduced cost, greater reliability, and greater maintainability.
Summary Accordingly, it is an object of the present invention to provide an improvement in microwave transmit/receive (T/R) modules. It is a further object of the present invention to provide an improvement in T/R modules used in connection with an active aperture of a pulse radar system.
And it is yet another object of the invention to provide an improved package for T/R modules utilized in a phased array radar system. And it is yet a further object of the invention to provide a low cost package for a transmit/receive module which results in reduced thermal impedance while providing high channel isolation between a plurality of discrete transmit/receive channels located side-by-side in a common housing structure.
The foregoing and other objects are achieved by a T/R module wherein a plurality, preferably two, discrete transmit/receive (T/R) channels are implemented in a single common package and having the capability of providing combined functions, control and power conditioning while utilizing a single multi-cavity, multilayer substrate comprised of high temperature cofired ceramic (HTCC) layers. The ceramic layers have outer surfaces including respective metallization patterns of ground planes and conductors as well as feedthroughs or vertical vias formed therein for providing three dimensional routing of both RF and DC signals so as to configure, among other things, a pair of RF manifold signal couplers which are embedded in the substrate and which transition to an RF interface including a multi-pin RF connector assembly at the front end of the package. The RF signal paths are enclosed in electrical shielding formed by parallel lines of vias and overlying stripline conductor elements. A DC and logic interface is located at the rear end of the package and includes means whereby DC power and control signals are connected to a plurality of active circuit components including application specific integrated circuit chips (ASICs) and monolithic microwave integrated circuit chips (MMICs) via spring contact pads. The MMICs, which include RF power amplification circuitry generate most of the heat, are located in multi-level cavities formed in the substrate and are bonded directly to a generally flat heat sink plate which is secured to the bottom of the substrate and acts as an efficient thermal interface to a cold plate type of external heat exchanger. DC power conditioning is also provided by a capacitive bank type of energy storage subassembly externally attached to the rear of the T/R module package for supplying supplementary power for peak power generation.
Further scope of applicability of the present invention will become apparent from the detailed description provided hereinafter. It should be noted, however, that the detailed description and specific example while indicating the preferred embodiment of the invention, is given by way of illustration only, since various changes, alterations and modifications coming within the spirit and scope of the invention will become apparent to those skilled in the art from this detailed description.
Brief Description of the Drawings
The present invention will become more fully understood when considered in conjunction with the accompanying drawings, which are provided by way of illustration only and thus are not meant to be limitive of the present invention, and wherein:
Figure 1 is an electrical block diagram broadly illustrative of a phased array radar system including a T/R module in accordance with the subject invention; Figures 2A-2D are perspective top, side and bottom plan views of a T/R module in accordance with the preferred embodiment of the invention;
Figure 3 is a perspective view of an energy storage capacitor bank located at the rear end of the T/R module shown in Figure 1;
Figure 4 is an exploded view of the capacitor bank shown in Figure 3;
Figures 5A, 5B, 5C and 5D disclose top, side and bottom plan views and an electrical schematic diagram of the circuit board assembly of the capacitor bank shown in Figure 4;
Figure 6 is a top plan view of the interior of the
T/R module package shown in Figure 1, and populated with components of each functional sub-system located therein; Figures 7A-7D are side, top, bottom and front plan views of an unpopulated T/R module package shown in Figure
1;
Figure 8 is a cross-sectional view of the T/R module package shown in Figure 7B, taken along the lines 8-8 thereof;
Figure 9 is a cross-sectional view of the T/R module package shown in Figure 7B, taken along the lines 9-9 thereof;
Figure 10 is a cross-sectional view of the T/R module package shown in Figure 7B, taken along the lines 10-10 thereof;
Figure 11 is an enlarged view of the left side portion of the cross section shown in Figure 8, and being further illustrative of the stack-up of the various HTCC ceramic layers located at the front portion of the T/R module package shown in Figure 7B; Figures 12A-12D are side, top, bottom and front plan views of an unpopulated T/R module package in accordance with the subject invention shown in Figures 7A-7D and now including a bottom heatsink plate attached thereto along with an RF coaxial connector assembly located at the front portion of the package;
Figure 13 is a cross-sectional view of the T/R module package shown in Figure 12B, taken along the lines 13-13 thereof; Figure 14 is a diagram further illustrative of the HTCC ceramic layers at the front portion of the package along with patterns of ground and signal vias forming an RF transition between certain layers;
Figure 15 is an electrical schematic diagram illustrative of the RF signal paths implemented within the package in accordance with the subject invention;
Figure 16 is a simplified electrical block diagram of the dual channel T/R circuit architecture which is implemented with the components shown in Figure 6; Figures 17A-17C are illustrative of the ground metallization pattern, via metallization and top metallization pattern formed in connection with HTCC layer 1 shown in Figure 14;
Figures 18A-18B are illustrative of via and top surface metallization pattern formed in connection with HTCC layer 2 shown in Figure 14;
Figures 19A-19B are illustrative of the via and top surface metallization pattern formed in connection with HTCC layer 3 shown in Figure 14; Figures 20A-20B are illustrative of the via and a ground metallization pattern formed in connection with HTCC layer 4 shown in Figure 14;
Figures 21A-21B are illustrative of the via and top surface metallization pattern formed in connection with HTCC layer 5 of Figure 14;
Figures 22A-22B are illustrative of the via and top surface metallization pattern formed in connection with HTCC layer 6 shown in Figure 14; Figures 23A-23B are illustrative of via and ground metallization pattern formed in connection with HTCC layer 7 shown in Figure 14;
Figures 24A-24B are illustrative of via and top surface metallization pattern formed in connection with HTCC layer 8 shown in Figure 14;
Figures 25A-25B are illustrative of via and top surface metallization pattern formed in connection with HTCC layer 9 shown in Figure 14; and
Figures 26A-26B are illustrative of via and ground metallization pattern formed in connection with HTCC layer 10 shown in Figure 14. Detailed Description of the Invention
Referring now to the drawings and more particularly to Figure 1, disclosed thereat is a block diagram broadly illustrative of an active aperture 1 for a radar system 2 including a plurality of phased array antenna elements 3 coupled to a plurality of identical dual channel T/R modules 10 by way of respective RF circulators 4. Each T/R module 10 includes a pair of RF transmit ports TX1 and TX2 and a pair of receive ports RXl and RX2 connected to separate antenna elements 3 and circulators 4 for implementing two separate and distinct T/R channels embodied within one common T/R module 10. Both T/R channels, moreover, share a common input port TXM from a transmit manifold 5 and a common output port RXM to a receive manifold 6 which form part of a common RF manifold for the system. The combined output from the receive manifold 6 is fed to the receiver section, not shown, of the radar system 2. RF pulses generated for transmission are fed to the transmit manifold 5 via an array driver 7. The six RF input/output ports TXl, TX2, RXl, RX2, TXM and RXM define an RF interface for the T/R module 10. The module 10, moreover, receives DC power from a DC source 8 and beam steering control signals are received from a beam controller 9 via a power/logic interface. All of these subsystems are under the control of a one or more microprocessors, not shown, located in the radar system 2.
Considering now the details of the preferred embodiment of the invention and as shown in Figures 2A-2D, the T/R module 10 exhibits an elongated relatively thin profile and implements a pair of discrete transmit/receive channels within a single common package including a multilayer substrate structure 12 comprised of a plurality of high temperature co-fired ceramic (HTCC) layers, to be described hereinafter, bonded together in a generally flat, rectangular configuration including a relatively wide front end portion 14 and a relatively narrow rear portion 16. The substrate 12 acts as a means for interconnecting a number of active and passive components which will be described hereinafter for implementing a dual T/R function for a phased array radar system. As shown in Figures 2A-2C, a flat metallized rectangular cover 18 fits over a metal ring frame, shown hereinafter, which is bonded to the top of the substrate 12 for protecting the electronic components located within the substrate as well as providing RF shielding therefor. A flat rectangular heat sink plate 20 is also bonded to the bottom of the substrate 12 as shown in Figure 2D and acts as a thermal interface for spreading and transferring heat generated within the module 10 to an external heat exchanger, e.g. cold plate, not shown. At the forward end of the substrate 12, as best shown in Figure 2A, are located six (6) discrete RF connectors located in a single connector subassembly 22 which can be easily plugged into the backside of an antenna array and which acts as an RF interface for all RF signals coupled to and from the module 10. These components are, moreover, brazed to the substrate 12 and form a package which is hermetically sealed.
All other electrical connections between the module 10 and external apparatus supplying, for example, DC power and control signals, are made through a DC/logic interface located at the other end of the substrate, with the heat sink plate 20 in between, and including a set of twelve (12) spring-like fingers 24x, 242 ...24ι2 (Figure 2C) mounted on a small generally rectangular circuit board 26 (Figures 5A-5C) located on the bottom of the module 10 behind the heat sink plate 20. The circuit board 26 forms part of DC power storage system comprising a capacitive bank subassembly 28 including five (5) electrical capacitors 30ι, 302 ... 305 and five (5) fuses 32:, 322 ... 325 (Figure 2A) , respectively connected in series with the capacitors 30ι ... 305 and whose purpose is to supply additional DC power to the module in a well known manner, during peak power operation.
The capacitive bank subassembly 28 is further shown in Figures 3, 4, and 5A-5D. In addition to the circuit board 26, the capacitive bank subassembly 28 additionally includes a flat cover member or "comb" 34 affixed to the bottom surface 36 of the circuit board 26 for protecting the fingers 24ι, 242 ...24ι2 (Figure 5C) and a relatively larger top member or "organizer" 38 affixed to the top surface 40 of the circuit board 26 for protecting the capacitors 30ι ... 305 and fuses 32ι ... 325 mounted thereon.
The members 34 and 38 are preferably comprised of molded plastic. As shown in Figure 4, the "comb" 34 includes an enlarged section 42 at one end which spans the width thereof and includes twelve relatively short identical parallel slots 44ι, 442, ... 44i2 which are adapted to fit over and around fingers 24ι, 242 ...24ι2 shown in Figures 5B and 5C. The "organizer" 38 includes a raised section 46, as shown in Figure 4, including five open cavities 48ι ... 485 which fit around the capacitors 30ι ... 305. Behind the cavities 48ι ... 485 are five smaller cavities 50ι ... 505 formed in a relatively thinner portion 52 which surround and protect the fuses 32ι ... 325.
Both the top and bottom surfaces 40 and 36 of the circuit board 26 include patterns of metallization in the form of conductor elements as shown in Figures 5A and 5C for implementing the DC/logic interface. With respect to the conductor pattern on the top surface 40 as shown in Figure 5A, there are ten equal sized relatively small rectangular conductors 52ι, 522, ... 52ι0 and one double width conductor 54. The conductor element 54 widens out to a larger section of metallization 56 which extends beneath the four larger capacitors 302 ... 305. One side of these capacitors are commonly connected to the area of metallization 56. A relatively small rectangular area of metallization 58 extends partially under the front end of the smaller capacitor 30ι and is connected thereto. The other end of capacitors 30ι "' 305 respectively terminate at five like areas of metallization 60ι, 602 ... 60 and connect one side of the capacitors 30ι ... 305 to an adjacent end of the respective fuses 32ι, " 325. The opposite end of fuse 32ι for the smaller capacitor 30ι connects a small area of metallization 61 which includes a connecting via through the back surface 36 of the board 26. The opposite ends of fuses 322 ... 325 connect to a common area of metallization 63 which also includes connecting vias to the back surface 36 of the circuit board 26 (Figure 5C) .
Referring now to the back surface 36 of the circuit board 26, the twelve metal spring finger connector elements 24ι, 242, ... 24i2 are in registration with the top conductor elements 52ι, ... 52ι0 and 54 and are mutually connected by electrical vias, not shown, through the board 26. Four areas of metallization 62, 64, 66 and 68 are additionally formed on the back surface 36 with the area of metallization 62 being connected to finger connector element 243, the area of metallization 64 being connected to connector element 244, the area of metallization 66 being commonly connected to a first pair of adjacent connector elements 245 and 266 while the area of metallization 66 is commonly connected to a second pair of connector elements 247, 248.
The T/R module 10 operates with two power supply potentials from respective external DC sources, not shown, namely a positive power supply voltage (+10.5VDC) and a negative power supply potential (-6.5VDC). The -6.5 volt negative supply voltage is connected to the module by way of finger element 244 and has a ground return by way of finger element 243. Respective connections thereof are made to the upper surface conductor element 524 and 523 of Figure 5A by vias, not shown, through the board 26. The two areas of metallization 62 and 64 couple across the series connection of the smaller capacitor 30ι and its associated fuse 322 by way of upper surface conductor elements 58 and 61.
The positive +10.5 volt supply voltage is commonly connected to connector fingers elements 247 and 248 where it is then applied to the upper conductor elements 54 and 56, which is common to one side of four parallely connected capacitors 302, 303, 304 and 305. A +10.5 volt ground return is provided from fingers 245 and 246 to the relatively large area of metallization 66 which connects back to conductor element 63 on the front surface 40
(Figure 5A) . This circuit configuration is further shown schematically in Figure 5D. The remaining fingers 24ι, 242 and 249 ... 24ι2 are utilized for logic input/output signals for the module as shown, for example, comprising the control signals VPROG, BIT, CMD-, CMD+, TR- and TR+ .
When placed against the substrate 12, the conductor elements 52ι,.„ 526, 54, 527 ... 52ι0 contact complementary opposing contact segments 55ι, ... 55ι0 on the substrate as shown, for example, in Figures 7C and 12C.
Considering now the structural details of the package of the T/R module, Figure 6 is generally illustrative of a structure that is referred to as a TWIN PAKTM because it is populated with two sets of semiconductor integrated circuit chips including, among other things, monolithic microwave integrated circuits (MMICs) and application specific integrated circuits (ASICs) for implementing two separate and independent T/R channels. While two T/R channels are contemplated for the preferred embodiment of this invention, it is conceivable that more than two channels could be implemented, if need be, with a more innovative design. Nevertheless, each of the two channels of the subject invention respectively include: a module controller 70, 72; a switch/phase shifter 74, 76; a pre or post amp/attenuator/switch/driver amplifier 78, 80; a low noise amplifier 82, 84; a receiver protector 86 and 88 and a power amplifier 90 and 92. Located between these elements are a shared gate regulator 94, a POWERFET switch 96, and power controller 98. These elements, moreover, are shown in the block diagram of Figure 16 and will be considered in greater detail hereinafter. The substrate 12, as further shown in Figures 7B and 12B, includes six multi-level cavities, three of which, as shown by reference numerals 100, 102 and 104, are located along one side edge of the substrate 12 and are used in connection with one of the T/R channels, while the other three cavities 106, 108 and 110 comprise like multi-level cavities along the other side edge of the substrate 12 and used in connection with the other T/R channel.
The cavities 100 ... 110 are, moreover, shown in the sectional views 8, 9, 10 and 13. With the exception of the forward cavities 104 and 110 in which is respectively located only in the power amplifier 90 and 92, the other cavities 100, 102 and 106, 108 include two or more integrated circuit components therein as shown in Figure 6. Such an arrangement results in separate isolated cavities for the RF gain stages in the input and output of the transmit circuitry. For example, the two rear cavities 100 and 106 share respective switch/phase shifter MMICs 74, 76 and post-amp/attenuator/switch/driver amplifiers MMICs 78, 80. The intermediate cavities 102 and 108 respectively include low noise amplifiers (LNA) 82, 84 and receiver protectors 86, 88. With respect to the module controllers 70 and 72, they do not reside in cavities, but are located on a top HTCC layer of the substrate 12. The two module controllers 70 and 72, the gate regulator 94 and power controller 98 are comprised of ASICs, while the phase shifter/switches 74, 76; the post amplifier/attenuator/switch/driver elements 78, 80; the low noise amplifiers 82, 84, and the two output power amplifiers 90, 92 comprise MMICs which reside in the cavities 100, 102, 104, 106, 108 and 110, and which are placed in direct contact with and bonded to the heat sink plate 20 as shown, for example, in Figure 14. While the heat sink plate 20 is preferably comprised of a copper tungsten alloy to enhance heat dissipation of the heat generated by the MMICs through the plate 20 to an external heat exchanger, not shown, other heat conducting metallic materials can also be used when desired, such as copper molybdenum or aluminum silicon carbide.
A metal ring frame as shown by reference numeral 112 is brazed on the top of the substrate 12 as shown, for example, in Figures 6 and 13 and is configured to border a major portion of the substrate 12 behind the front end portion 14 so as to encircle the six cavities 100, 102 ... 110 as well as the regions including the module controllers 70 and 72 and the shared circuit components 94, 96 and 98 residing in the center of the substrate on either side of the T/R channels. Its purpose is to receive and support the flat cover member 18 shown in Figures 1 and 2A and provide isolation and RF shielding from respective elements.
Figures 7A-7D are intended to illustrate the construction of the substrate 12 in its unpopulated state, and without an RF connector 22 assembly and heat sink plate 20. Figures 12A-12D, on the other hand, are intended to show the same unpopulated structure of the substrate 12, but now also including the heat sink plate 20 and the RF connector assembly 22. The stippling is intended to denote surfaces which include areas of exposed metallization, e.g. gold. Figure 7C is illustrative of the exposed bottom surface 114 of the substrate 12 and includes openings therein 116, 118 ... 126 and which correspond to the shape of the cavities 100, 102 ... 110 shown in Figure 7B looking from the top. The surface 114, moreover, comprises the lowermost surface of the lowermost layer 13ι of a plurality of stacked HTCC layers 13: ... 13ι5 shown in Figures 8-11, 13 and 14. The metallization pattern comprises a ground plane of metallization 128 including the two input conductor segments 553 and 555 and the isolated input/output conductor segments 55χ, 552/ 554, 556 ... 55ι0 which mate with the conductor segments 52ι "" 52δ, 54, 527 ... 52ιo of the capacitor bank connector plate 26 as shown, for example, in Figure 5A. It can be seen that conductor segment 553 of Figure 7C and segment 523 of Figure 5A form a common ground connection along with segment 555 of Figure 7C and segments 525, 526 of Figure 5A.
Figure 7D shows the face 130 of the front end portion 14 of the substrate 12 including six (6) isolated circular segments of metallization 132ι, 1322 ... 1326 which define the pin location of six (6) aligned blind mate press on connectors 134χ, 1342 ... 1346_ included in the connector assembly 22, as further shown in Figure 12D, and enclosed in an elongated generally rectangular shroud 136.
The connector assembly 22 results in an in-line connector assembly including two separate transmit (Tx) connectors 1342 and 1346, two separate receive (Rx) connectors 134ι and 1345 for individual connection to antenna elements of an array, but only two manifold connectors 1343 and 1344 which share connection to a transmit and receive manifold and which allows the module 10 to be easily plugged into the array during assembly and thereafter removed when required.
It can be seen with reference to Figure 12B that the inner surface of the heat sink plate 20 also includes metallization which covers the cavity openings 116, 118 ... 126 of Figure 7C. It is this surface on which all of the heat generating MMICs located in the six cavities 100, 102 ... 110 are mounted.
Referring now to the cross-sectional views of Figures 8-11 and Figures 13, 14, shown thereat is the multi-level, configuration of the high temperature co-fired ceramic (HTCC) substrate 12. As shown in Figure 11, for example, the substrate 12 is comprised of fifteen contiguous layers 13]., 132 ... 13i5 of HTTC material, ranging in thickness between .006 in. to .020 in. and wherein layers 13ι through 1310 are used to form the six cavities 100, 102, 104, 106, 108 and 110.
The multi-level structure of the substrate 12 as shown in Figure 14 permit passive components to be located within the cavities on layer or steps 134, for example, and for implementing wire bond connections between chips at layer 132 and for providing connections to the MMICs located on the heat sink plate 20. In Figure 14, reference numeral 90 represents the RF power output amplifier MMIC 90 located in cavity 104. The layer 13ι0 comprises a layer upon which the power controller ASIC 98 is located. Also layer 13ι0 is the layer upon which the ring frame 112 member (Figure 13) and connector pins 138ι ... 1386 of a blind mate press-on connector assembly 22 are brazed. The connector pins 138ι "' 1386 comprise elements which are manufactured and supplied by Gilbert Engineering, Inc. of Phoenix, Arizona in forming what is referred to as a Gilbert press-on or "GPPO" connector. The five uppermost layers 13u "' 13ι5 shown at the right on Figure 14, comprise what is referred to as "dummy" layers and form the forward portion 14 of the substrate 12. The substrate layers 13ι ... 13ι0 provide the ability to implement 3-D routing of both RF signals and DC signals within the substrate 12 as well as embedding a pair of RF manifold couplers therein. RF routing and transitions comprise coupling the inputs and outputs from the six pin connector assembly 22 and implementing a well matched structure up to all the MMICs located in the cavities 100 ... 110. Shielded 3-D routing is implemented within the substrate 12 and results from the layers 13ι '" 13ιo being comprised of contiguous discrete dielectric layers, each with its own pattern of ground plane and vertical feed- throughs or vias, along with respective stripline conductor patterns formed on the top surface thereof as will be shown hereinafter. RF signals enter and leave the module 10 by means of the connector assembly 22.
Connector assembly 22 includes six like RF coaxial connectors 134ι ... 1346, including pins 138ι ... 1386, arranged in linearly (Figure 12D) within and across the shroud member 136. In Figure 14, the connector pin 138i is shown connected to a stripline conductor 140 on the top of the HTCC layer 1310. Stripline conductor 140 extends inwardly where it connects to a vertical via 142 which descends to a length of stripline conductor 144 on the top of layer 136. Immediately below conductor 144 on top of layer 135 is a length of stripline conductor 146 which extends under conductor 144. Such an arrangement permits RF coupling between conductors 144 and 146 and is intended to illustrate the concept of two RF manifold couplers, one of which acts as a signal splitter and one of which acts as a signal combiner, which are embedded in the substrate 12 and will be described hereinafter. Further as shown in Figure 14, stripline conductor 146 connects to a vertical via 148 which descends to the top of layer 132 and stripline conductor 150. At the outer end of conductor 150 is a bond wire member 151 which connects the MMIC 90. A stripline conductor element 149 which acts as a capacitive stub is also shown located on the top of layer 13ι directly beneath the bond wire connection of member 151 to conductor 150. Isolation and shielding for the RF coupler configured by stripline conductors 144 and 146 are further provided by upper and lower ground planes 152 and 154 including multiple vertical vias 156, 158 and 162 terminating the top of layers 134 and 137, respectively.
Also, as shown in Figure 14, the shroud 136 is coupled to three ground planes 164, 166 and 168 which are further interconnected by multiple vertical vias 170, 172 and 174. This in combination with the metal alloy plate 20, provides shielding for the signals passing to and from the RF connector assembly 22. Achieved thereby is an RF structure including a connector to stripline section, a stripline to stripline section, a coupler section and a stripline to MMIC section.
Minimal RF output routing is obtained by the configuration of the invention shown in Figure 14. The benefit obtained results from the fact that about 1 to 2 dB of losses can be produced by each inch of RF routing from a power amplifier to the RF interface through one or more module layers. Such a loss would drop the output RF power from 100% nominal to about 80% with use of alumina ceramic dielectric as substrate and layer material, or to about 63% with use of common black ceramic.
Referring now to Figures 17A, 17B, 17C through 26A and 26B, wherein like reference numerals refer to common elements, shown thereat are the vertical vias formed through each of the dielectric HTCC layers 13ι ... 13ι0 and the respective stripline conductor metallization patterns formed on the top surfaces thereof.
Considering first Figures 17A, 17B and 17C, depicted thereat is the lowermost layer 13ι of the substrate 12 and one which includes a ground plane 128 (Figure 7C) , the face-up side of which is shown in Figure 17A along with the DC logic conductor interface elements 55ι ... 55ι0. Generally rectangular unmetallized areas 116 ... 126 which define openings for the six cavities 100, 102 ... 110 are also shown in Figure 17A. This same pattern of openings also exists in the upper HTTC layers 132 ... 13ι0.
Figure 17B discloses the pattern of vias fabricated vertically through HTCC layer 13ι. The circular via patterns 180, 182, 184 ... 198, 200 are illustrative of a plurality of cylindrical vertical via patterns which can be seen in combination with the upper ceramic layers 132 and 133 such as Figures 18A and 19B to form cylinder-like shielded conduits for RF signal carrying vias centralized in the circular patterns of vias and transitioning vertically between layers. Pairs of mutually parallel lines of vias 202, 204 ... 216, 218 represent shielding type passageways for signal carrying stripline conductors located in layer 132 (Figures 18A, 18B) above layer 13ι. The top surface of layer 13ι as shown in Figure 17C includes a stripline metallization pattern which acts in concert with the underlying lines of vias 202 ... 218 to form a bottom channelized RF shielding layer for the signal carrying conductors located above on layer 132 along with stripline elements 222, 224 ... 236, 238. Referring now to layer 132 and Figures 18A and 18B, the arrangement of vertical vias shown in Figure 18A is substantially the same as that shown in Figure 17A, with the exception of an absence of vias at the area of reference numeral 240. The pattern of metallization of Figure 18B matches that of Figure 17C, but now also includes, for example, RF signal carrying stripline conductors 240, 242 ... 264, 266, with conductors 240, 242, 250, 254, 256, 258, 260, 262, and 266 terminating in vertical vias 241, 251, 255, 257, 259, 261, 263, 365 and 267. Borders of metallization 268, 270 ... 278, 280 surround the cavity areas 116 ... 126 (Figure 17A) . It is important to note that the stripline conductors 250, 254 and 266 feed out to RF connectors 134ι(RXl), 1342(TX1) and 1346(TX2) shown in Figure 12D by means of vertical vias 251, 255 and 267.
With respect to the third layer 133 shown in Figures 19A and 19B, its pattern of vertical vias as shown in Figure 19A also matches the via patterns of Figures 17B and 18A, particularly with respect to the parallel line pairs of vias 202 ... 218. The top surface of metallization of Figure 19B includes substantially the same stripline pattern shown in Figure 17C but with an extra area of metallization 281 and thus acts as a top channelized shielding layer thereby implementing a shielded outer conductor or conduit for the signal carrying conductors located in layer 132" The bottom three layers 13ι, 132, and 133 of HTCC material thus implement one of two levels of RF routing and one for routing RF signals between the various MMICs in the cavities 100 ... 110 and the connector assembly 22 (Figures 12D)
Proceeding upwards in the substrate 12, layer 134 as shown in Figures 20A and 20B comprises an HTCC layer implementing a first internal ground plane. Its pattern of vias, as shown in Figure 20A, substantially matches the via pattern shown in the underlying layer 133 (Figure 19A) . The upper surface of layer 134 (Figure 20B) comprises a ground plane of stripline as shown by reference numeral 282, along with a plurality of circular openings within which are located vias 241, 243 ... 267, as shown. These vias match the underlying like numbered vias in Figure 19B.
Next, the intermediate layers 135, 136 and 137, in addition to including specific patterns of conductors and vias, also implement a pair of RF signal couplers which connect to both T/R channels and which results in eliminating two relatively expensive GPPO manifold connectors. An example of how such a coupler is fabricated in the subject invention is shown in Figure 14 with reference to the stripline conductors shown by reference numerals 144 and 146.
Referring now to the fifth HTCC layer 135 as shown in Figures 21A and 21B, shown in Figure 21A is a vertical via pattern of vias and stripline which also includes, inter alia, the circular via patterns 180, 181, 182 ... 198, 200, but also now includes new parallel line pairs of vias 284, 286, 288, and 290, with pairs 286, 288 and 290 terminating in respective additionally circular via patterns 292, 294 and 296 located at the RF connector end of the substrate.
With respect to the metallization pattern on the top surface of layer 13s as shown in Figure 21B, it includes pairs of parallel stripline shield conductors 298, 300 and 302 over the parallel lines of vias 284, 286 and 288 shown in Figure 21A. Also, shielding striplines 304, 306 ... 312, 314 are again formed around the openings for the cavities 102, 104 ... 110. Centrally located on layer 135 are two underlying stripline segments 316 and 318 of two RF signal couplers, one a transmit manifold coupler 320 which acts as an RF signal splitter, and the other a receive manifold coupler 322, which acts as an RF signal combiner, and whose respective overlaying stripline segments are shown by reference numerals 324 and 326 in Figure 22B (layer 136) . One side of transmit manifold coupler segment 316 is connected to conductor 328 and via 259 while the opposite side connects to an elongated conductor 330 which passes through conductor pair 302 to a vertical via 334 in the circular via pattern 294 and which connects to RF connectors 1344 (Figure 12D) .
One side of receive manifold coupler segment 322 connects to conductor 336 and via 184 while the opposite side thereof connects to an elongated conductor 338 which passes through conductor pair 300 to a vertical via 340 in circular via pattern 292 and which then connects to RF connector 1343 in Figure 12D. Figure 21B also depicts a shield conductor pair 341 which mutually shares a conductor with adjacent shield conductor pair 302. A vertical via 342 is also now provided in circular via pattern 296.
Considering now layer 136, the via pattern of layer 13β illustrated in Figure 22A is similar to that in the underlying layer 135 shown in Figure 21A. The stripline conductor patterns on the top surface of the layer 136 again operate as shielding elements for implementing shielding enclosures for the underlying RF conductors 300 and 330 shown in Figure 2IB as well as an RF conductor line 344 connected between via 179 and one side of transmit manifold coupler segment 324. Now an RF conductor line 346 for the received signal (RX2) of the second T/R channel is connected between via 265 and vertical via 342 in circular via pattern 296 at the RF connector end of the substrate 12. Further as shown in Figure 22B, one side of receive manifold coupler segment 322 connects to conductor 348 and via 257 while the other side connects to conductor 350 and via 263.
Thus layers 135 and 136 which overlay the ground plane metallization 282 of layer 134 as shown in Figure 20B comprise a second level of RF routing which is primarily used for routing RF signals to and from the manifold couplers 320 and 322; however, as noted above, layer 136 also routs the RF receive signal from the antenna array and connector assembly 22 (Figure 12D) to the low noise amplifier 84 located in cavity 108.
Layer 137 comprises a second ground plane layer. It includes a via pattern as shown in Figure 23A which substantially matches the via pattern in the underlying layer 136 shown in Figure 22A. Figure 23B is illustrative of the metallization pattern formed on the top of layer 137 and comprises a ground plane metallization 352 but now includes six (6) circular openings for the six vertical RF connector vias 251, 255, 267, 334, 340 and 342. The ground plane metallization 352 also includes seven (7) isolation stubs 354, 356, ... 364, 366 which are located between the six(6) RF connectors 134ι ... 1346 (Figure 12D) .
The upper HTCC layers 138, 139 and 13χo provide a level of routing of DC power and logic control signals between the various MMICs and ASICs as well as providing for connection of the pins 138ι, 1382 ... 1386 of the RF connectors 134ι, 1342, ... 1346 of the RF connector assembly 22 at the front portion 14 of the substrate 12.
With respect to the ceramic layers 138, and 139, the pattern of vertical vias as shown in Figs. 24A and 25A are similar but now include six (6) arcuate via patterns 368, 370 ... 376, 378 forward of the vias 251 ... 267 at the connector end of the substrate. However, the top surfaces thereof have selectively different patterns of stripline conductor metallization as shown in Figs 24B and 25B. The upper surface of metallization of layer 138 as shown in Figure 24B includes a conductor pattern of stripline conductors, isolation borders, as well as seven (7) connector pin isolation stubs 380 ... 402 which match the stubs 354 ... 366 of layer 137 (Figure 23B) . The via pattern for layer 1310 as shown in Figure 26A is similar to the via pattern shown in Figure 25A for the underlying layer 139; however, in addition to the arcuate via patterns 368 ... 378 included therein are vias 404 ... 414 aligned with vias 251 ... 267 and which are provided for mating with six stripline conductor elements 416 ... 426 as shown in Figure 26B. The six connector pins 138ι, 1382 ... 1386 are brazed to the stripline conductor elements 416 ... 426 in the fabrication of the substrate 12.
A set of seven (7) pin isolation stubs 430 ... 442 as shown in Figure 26B are located between and insulated from the pin connector strips 416 ... 426. A ground plane is further provided by a large metallization area shown by reference numeral 444, including openings formed therein for accommodating the MMICs and ASICs located in the cavities 100 ... 110 of the substrate 12. Having considered the structural details of HTCC layers 13ι ... 13ι0, the RF signal paths implemented thereby are shown in the block diagram of Figure 15. Returning now to Figure 15, it can be seen that RF signals for two discrete T/R channels are coupled to and from the substrate 12 via connector assembly 22 located at one end of the substrate. DC power and logic control signals are applied to the substrate 12 at the other end as shown. The RF signal paths depicted in Figure 15 can be found on the top surface of layer 132 as shown in Figure 18B and the top surfaces of layers 135 and 136 as shown in Figures 21B and 22B, respectively, and where, as noted before, RF routing is broken into two sections, a lower section including layers 13ι, 132, and 133 and an upper section including layers 135 and 136. Layer 132 of the bottom RF section is used primarily for routing RF signals between MMICs and to/from the connector assembly 22, while layers 135 and 136 of upper section are used for the implementation of the two manifold couplers 320 and 322. As noted above, layer 136 is also used for routing the RF received signal for one of the channels. Referring also back now to Figure 16, shown thereat is the electrical architecture of the dual channel transmit/receive RF circuitry located on and within the substrate 12. The circuitry for each channel is substantially like that shown and described in U.S. 5,745,076, Turlington et al in that the same circuit components are respectively used in each channel for gain trim, phase shifting and intermediate power amplification during both the transmit modes of operation. However, each channel operates independently of the other, while sharing in a unique manner not only the transmit and receive manifolds by way of the RF couplers 320 and 322, but also the power and operation of the gate regulator 94, the POWERFET switch 96, and the power controller 98. Accordingly, and as shown in Figure 16, each channel includes: a receiver protector (R/P) element 86, 88; a low noise amplifier 82, 84 including two stages of amplification; an RF switch and phase shifter (SW/PHS) 74, 76 including a single pole double throw RF switch and a digitally controlled phase shifter; an amplifier/gain trim attenuator/switch/driver amp (AMP/ATTN/SW/DVR) 78, 80 including three stages of pre amp or post amp amplification, a second single pole, double-throw switch located between a pair of digitally controlled gain trim attenuators and two stages of driver amplification; and a power amplifier 90, 92 including three stages of RF power amplification.
Beam control signals are fed from the beam steering controller 9 (Figure 1) to separate module controllers 70 and 72 so as to respectively provide phase and amplitude control over RF transmit and receive signals in the respective T/R channels. However, the module controllers 70 and 72 preferably operate on a limited basis of shared module control via the power controller 98 by providing crossover channel control so that in the event one of the module controllers fails, the other module controller takes over. Further, either module controller 70 or 72 will shut down the entire module 10 upon the detection of certain conditions, in order to prevent faulty module operation from adversely affecting the accuracy of overall beam control.
The use of a multi-layer substrate which may be implemented as an MLCC such as an HTCC structure provides a number of attendant advantages in terms of design flexibility, performance and at lower cost. The multi- layer nature of the structure permits isolated crossovers of both RF and DC, due to the fact that ground planes are located between signal lines. The overall density of the assembly is increased due to both the ability to integrate certain passive microwave components, and the ability to perform 3-D routing of both RF and DC signals.
In the present invention, fewer modules need to be assembled and tested per application site, thereby providing a first order of savings. In addition, the T/R modules 10 can be structured for ease of module assembly and ease of assembly of the module into the antenna array. As a result of improved T/R circuitry architecture and improved layout architecture achieved, the invention further enables performance and cost improvements to be realized in a multi-channel T/R module which can be conveniently plugged into an antenna assembly while making electrical and heat sink connections simultaneously between the module and the assembly. Importantly, RF connections are made with high stability against vibration, thereby supporting quality RF signal processing, and the heat sink connection is made with large surface contact area, thereby supporting higher heat dissipation, reduced rise in junction temperatures of module semiconductor devices, and higher module RF power capability.
Having thus shown and described what is at present considered to be the preferred embodiment of the invention, it should be noted that the same has been made by way of illustration and not limitation. Accordingly, all modifications, alterations and changes coming within the spirit and scope of the invention as set forth in the appended claims are meant to be included.

Claims

1. A transmit/receive (T/R) module for an active aperture of a radar system, comprising: a substrate having two opposing end regions, an RF interface located at one of said end regions; a DC/logic interface located at the other of said end regions; a plurality of cavities formed in the substrate; an outer heat sink plate bonded to the substrate and covering said plurality of cavities; at least one T/R channel circuit implemented on said substrate and including a plurality of circuit components; wherein a selected number of said plurality of circuit components are located in said cavities and are mounted directly on the heat sink plate.
2. A T/R module according to claim 1 wherein said at least one T/R channel circuit comprises a plurality of T/R channel circuits.
3. A T/R module according to claim 1 wherein said at least one T/R channel circuit comprises two T/R channel circuits .
4. A T/R module according to claim 1 wherein said substrate comprises a co-fired multi-layer ceramic structure .
5. A T/R module according to claim 1 wherein said substrate comprises a multi-layer laminated or molded conductor/dielectric structure.
6. A T/R module according to claim 1 and additionally including a ring frame member bonded on the top of the substrate and a top cover member bonded on the ring frame member for forming a sealed package and mutually isolating said cavities from each other.
7. A T/R module according to claim 1 wherein said RF interface includes RF connector means for coupling RF signals to and from said T/R channel circuits.
8. A T/R module according to claim 7 wherein said connector means comprises a plurality of blind mate press- on RF connectors arranged in a row across an end face of the substrate.
9. A T/R module according to claim 1 wherein said DC/logic interface includes means connected to the substrate for supplying additional power to the T/R channel circuit during peak power operation for RF pulse transmission.
10. A T/R module according to claim 9 wherein said means for supplying additional power comprises a bank of capacitors which are chargeable from an external DC power source.
11. A package for a transmit/receive (T/R) module, comprising: a common substrate for two discrete T/R channels, having a relatively thin profile and being comprised of a plurality of laminated ceramic layers, each having a predetermined pattern of electrical vias therethrough and a predetermined pattern of metallization at least on one surface thereof, for providing three dimensional routing of signals and power between the layers of the substrate and further including two like sets of multilevel cavities formed therein, one set for each said T/R channel, arranged side by side and in which one or more active circuit components are respectively located; a ring frame member located on top of said substrate, bordering a major portion of the outer periphery of the substrate as well as encircling the two sets of cavities; a cover member located on said ring frame, said cover member enclosing and mutually isolating the cavities of said two sets of cavities from each other; a heat sink plate on an underside surface of the substrate and also covering an area including the two sets of cavities, said active circuit components being in direct contact with said heat sink plate and which thereby provides a thermal interface to an external heat exchanger; connector means including a plurality of discrete signal connectors located at one end of the substrate for independently coupling RF signals to and from both said T/R channels; and means at the opposite end of the substrate for receiving externally generated DC power and operational logic control signals for said active circuit components of both said T/R channels.
12. A package according to claim 11 wherein said cover member is bonded to said ring frame member and wherein said ring frame member, said heat sink plate, and said connector assembly are bonded to said substrate so as to form a hermetically sealed T/R package.
13. A package according to claim 12 wherein said cover member includes a generally flat outer surface.
14. A package according to claim 12 wherein said heat sink plate includes generally flat inner and outer surfaces and wherein said active circuit components are located on said flat inner surface of the heat sink plate.
15. A package according to claim 11 wherein said plurality of ceramic layers are comprised of high temperature cofired ceramic (HTCC) .
16. A package according to claim 15 wherein each set of cavities includes three mutually aligned multi-level cavities, said cavities having intermediate levels for providing external connections to the respective active circuit components located in the cavities and for mounting passive circuit components thereon.
17. A package according to claim 15 wherein a first cavity of each said set includes therein a first active circuit component implementing an RF preamplifier in a transmit mode and postamplifier in a receive mode, a signal attenuator, a switch and an RF driver amplifier and a second active circuit component implementing another RF switch and a phase shifter, wherein a second cavity of each said set includes therein an active circuit component implementing a low noise amplifier, and wherein a third cavity of each said set includes an active circuit component implementing an RF output power amplifier.
18. A package according to claim 17 wherein said active circuit components comprise monolithic microwave integrated circuits (MMICs) .
19. A package according to claim 17 and additionally including a pair of module controllers located on said substrate for controlling said two T/R channels.
20. A package according to claim 17 and additionally including a pair of non-cavity regions at said opposite end of said two sets of cavities for locating thereat a respective active circuit component implementing module controllers for the two T/R channels.
21. A package according to claim 20 wherein the active circuit component at said non-cavity regions comprise application specific integrated circuits (ASICs) .
22. A package according to claim 20 and further including a non-cavity region between said two sets of cavities and said pair of non-cavity regions for locating thereat active circuit components for implementing a gate regulator, a DC power controller, a power switch which are commonly utilized by both said T/R channels.
23. A package according to claim 15 and wherein said connector means comprises an RF connector assembly including a first pair of RF input and output connectors for one of said two T/R channels, a second pair of RF input and output connectors for the other of said T/R channels, an RF receive manifold connector for both said T/R channels, and an RF transmit manifold connector for both said T/R channels.
24. A package according to claim 23 wherein all of said connectors are linearly arranged side by side and located in a common shroud.
25. A package according to claim 24 wherein said connectors comprise blind mate connectors for facilitating relatively easy connection to an antenna array.
26. A package according to claim 25 wherein said blind mate connectors comprise press-on connectors.
27. A package according to claim 23 and wherein said plurality of ceramic layers of HTCC includes at least two sets of layers for providing at least two levels of RF signal routing in the substrate and at least one set of layers for providing at least one level of DC power and control signal routing in the substrate.
28. A package according to claim 27 and wherein said plurality of layers of HTCC include a layer between said sets of layers having an electrical shielding or ground plane metallization pattern.
29. A package according to claim 27 wherein one set of said two sets of layers providing RF signal routing couples RF signals between predetermined RF input and output connectors of said connector assembly and predetermined active circuit components of said T/R channels.
30. A package according to claim 29 wherein the other set of said two sets of layers include a first and a second stripline RF signal coupler formed between two adjacent layers of said other set of layers for respectively coupling RF signals between said receive manifold connector and said transmit manifold connector and predetermined active components of said T/R channels.
31. A package according to claim 30 wherein said two sets of layers providing two levels of RF signal routing comprise two adjacent levels of signal routing below said one set of layers providing said one level of DC power and control signal routing.
32. A package according to claim 27 wherein said two sets of layers providing RF signal routing include multiple pairs of parallel lines of electrical vias and respective stripline conductors overlaying said parallel lines of electrical vias for providing a predetermined number of shielded conduits surrounding a selected number of RF signal stripline conductors along their length.
33. A package according to claim 27 wherein said layers include one or more generally circular patterns of electrical vias and an electrical via centralized therein for providing respective shielded conductor crossovers between layers for effecting three dimensional routing of signals and power within the substrate.
34. A package according to claim 11 wherein said means at the opposite end of the substrate for receiving DC power and logic control signals includes a metallization pattern on the outer surface of a lowermost layer of said substrate.
35. A package according to claim 34 wherein said means for receiving externally generated DC power and control signals additionally includes a spring contact assembly electrically coupled to said metallization pattern and connectable to an external source of DC power and an external source of T/R channel control signals.
36. A package according to claim 11 and additionally including external energy storage means connected to said means for receiving externally generated DC power for supplying additional DC power to the package.
37. A dual channel transmit/receive (T/R) module exhibiting a relatively thin profile, comprising: a common substrate for two discrete T/R channels, including a plurality of laminated ceramic layers, each having a predetermined pattern of electrical vias therethrough and a predetermined pattern of metallization at least on one surface thereof, for providing three dimensional routing of signals and power between the layers of the substrate and further including two like sets of multilevel cavities formed therein, one set for each said T/R channel, arranged side by side and in which one or more active circuit components are respectively located; a ring frame member bonded to the top of said substrate, said ring frame member bordering a major portion of the outer periphery of the substrate as well as encircling the two sets of cavities; a cover member bonded to said ring frame member and covering an area including the two sets of cavities; a heat sink plate bonded to the underside surface of the substrate and also covering an area including the two sets of cavities, said active circuit components being in direct contact with said heat sink plate and which thereby provides a thermal interface to an external heat exchanger; a unitary RF connector assembly including a plurality of discrete signal connectors located at one end of the substrate for independently coupling RF signals to and from said T/R channels; a power and logic interface at the opposite end of the substrate for coupling DC power and operational control signals to said active circuit components located on the substrate; and energy storage means located at the opposite end of the substrate for supplying supplementary DC power to said active circuit components located on the substrate.
38. A dual channel T/R module according to claim 37 wherein said plurality of ceramic layers are comprised of high temperature cofired ceramic (HTCC) material.
39. A dual channel T/R module according to claim 38 wherein said ring frame member and said cover member are comprised of electrically conductive material and wherein said cover member is bonded on said ring frame member so as to form a seal thereat and wherein said ring frame member, said heat sink plate and said connector assembly are brazed on said substrate so as to form a hermetically sealed T/R package.
40. A dual channel T/R module according to claim 39 wherein said cover member includes a generally flat outer surface and wherein said heat sink plate includes generally flat inner and outer surfaces and wherein said active circuit components are located on said flat inner surface of the heat sink plate.
41. A dual channel T/R module according to claim 37 wherein said energy storage means comprise a plurality of storage capacitors.
42. A dual channel T/R module according to claim 41 wherein said plurality of capacitors are located in a support housing attached to said substrate.
43. A dual channel T/R module according to claim 42 wherein said DC power includes at least one DC supply voltage and wherein said plurality of capacitors includes at least one capacitor for said at least one DC supply voltage.
44. A dual channel T/R module according to claim 38 wherein each set of cavities includes three multi-level cavities having intermediate levels for providing external wire connections to the respective active circuit components located in the cavities and for mounting passive circuit components thereon.
45. A dual channel T/R module according to claim 44 wherein each set of three cavities are mutually aligned along a side edge of the substrate and wherein a first cavity of each said set includes therein a first active circuit component implementing an RF preamplifier in a transmit mode and post amplifier in a receive mode, a signal attenuator, a switch and an RF driver amplifier and a second active circuit component implementing another RF switch and a phase shifter, wherein a second cavity of each said set includes therein an active circuit component implementing a low noise amplifier, and wherein a third cavity of each said set includes an active circuit component implementing an RF output power amplifier.
46. A dual channel T/R module according to claim 45 wherein said active circuit components comprise monolithic microwave integrated circuits (MMICs) .
47. A dual channel T/R module according to claim 45 and additionally including a pair of non-cavity regions at said opposite end of said two sets of cavities for locating thereat a respective active circuit component implementing module controllers for the two T/R channels.
48. A dual channel T/R module according to claim 47 wherein the active circuit component at said non-cavity regions comprise application specific integrated circuits (ASICs) .
49. A dual channel T/R module according to claim 47 and further including a non-cavity region between said two sets of cavities and said pair of non-cavity regions for locating thereat active circuit components for implementing a gate regulator, a DC power controller, a power switch which are commonly utilized by both said T/R channels .
50. A dual channel T/R module in accordance with claim 49 wherein said active circuit components at said non-cavity regions comprise application specific integrated circuits (ASICs)
51. A dual channel T/R module according to claim 37 and wherein said connector assembly comprises a first pair of RF input and output connectors for one of said two T/R channels, a second pair of RF input and output connectors for the other of said T/R channels, an RF receive manifold connector for both said T/R channels, and an RF transmit manifold connector for both said T/R channels, and wherein said connectors comprise blind mate connectors for facilitating relatively easy connection to an antenna array.
52. A dual channel T/R module according to claim 51 wherein all of said connectors are mutually aligned and located in a common shroud.
53. A dual channel T/R module according to claim 52 and wherein said plurality of ceramic layers of HTCC includes two sets of layers for providing two levels of RF signal routing in the substrate and one set of layers for providing DC power and control signal routing in the substrate and further including a layer of HTCC between said sets of layers having an electrical shielding or ground plane metallization pattern.
54. A dual channel T/R module according to claim 53 wherein one set of said two sets of layers providing RF signal routing couples RF signals between predetermined RF input and output connectors of said connector assembly and predetermined active circuit components of said T/R channels wherein the other set of said two sets of layers include a first and a second stripline RF signal coupler formed between two adjacent layers of said other set of layers for respectively coupling RF signals between said receive manifold connector and said transmit manifold connector and predetermined active components of said T/R channels.
55. A dual channel T/R module according to claim 54 wherein said two sets of layers providing two levels of RF signal routing comprise two adjacent levels of signal routing below said one set of layers providing said one level of DC power and control signal routing.
56. A dual channel T/R module according to claim 53 wherein said two sets of layers providing RF signal routing include multiple pairs of parallel lines of electrical vias and respective stripline conductors overlaying said parallel lines of electrical vias for providing a predetermined number of shielded channels surrounding respective RF signal stripline conductors located therein wherein said plurality of layers selectively include one or more generally circular patterns of electrical vias and an electrical via centralized therein for providing respective shielded conductor crossovers between layers for effecting three dimensional routing of signals and power within the substrate.
57. 7An electrical energy storage assembly for supplying supplementary DC power to a transmit/receive (T/R) module during peak power operation, comprising: a base member comprised of electrical insulation material and having a pair of opposed mounting surfaces; a first plurality of electrical contact elements located on one of said mounting surfaces for connection to an electronic circuit assembly of the T/R module ; a second plurality of electrical contact elements located on the other of said mounting surfaces for connection to at least one external DC power source and an external source of control signals; a plurality of electrical vias through the base member for selectively interconnecting the first and second plurality of electrical contact elements; a plurality of electrical energy storage elements mounted on one of said mounting surfaces; and wherein one side of said energy storage elements are connected to predetermined ones of said first plurality of contact elements on one of said mounting surfaces and wherein the other side of said energy storage elements are connected to predetermined ones of said second plurality of contact elements on the other of said mounting surfaces.
58. An electrical energy storage assembly according to claim 57 wherein said energy storage elements comprise electrical capacitors.
59. An electrical energy storage assembly according to claim 57 wherein said base member comprises a relatively thin flat plate member.
60. An electrical energy storage assembly according to claim 59 wherein said first plurality of electrical contact elements comprise a pattern of conductor segments.
61. An electrical energy storage assembly according to claim 60 wherein said second plurality of electrical contact elements comprise a set of mutually parallel resilient contact members.
62. An electrical storage assembly according to claim 61 wherein said resilient contact members comprises a set of bowed finger contact elements having a folded back end portion.
63. An electrical storage assembly according to claim 62 and additionally including a protective member attached to the base member for protecting the end portion of each said finger contact element.
64. An electrical storage assembly according to claim 63 wherein said protective member comprises a generally flat member of a predetermined thickness and including a set of parallel apertures therein and through which said end portions protrude.
65. An electrical storage assembly according to claim 60 where a predetermined number of said electrical storage elements are connected in parallel between said pattern of stripline conductor segments and said set of resilient contact members.
66. An electrical storage assembly according to claim 65 wherein said electrical energy storage elements comprise storage capacitors.
67. 7An electrical storage assembly according to claim 66 and additionally including a respective electrical fuse connected in series with each of said storage capacitors.
68. An electrical storage assembly according to claim 67 and additionally including a protective member attached to the base member for protecting said storage capacitors and said fuses.
69. An electrical storage assembly according to claim 68 wherein said protective member comprises a cowling type of member which fits around said storage capacitors and said fuses.
70. An active aperture for a radar system, comprising: an array of antenna elements; and an array of dual channel transmit/receive (T/R) modules for transmitting RF signals to and receiving RF signals from said array of antenna elements.
71. An active aperture according to claim 70 wherein said array of antenna elements comprises a phased array.
72. An active aperture according to claim 71 wherein each T/R module includes: a common substrate for two discrete T/R channels, including a plurality of laminated ceramic (HTCC) layers, each having a predetermined pattern of electrical vias therethrough and a predetermined pattern of metallization at least on one surface thereof, for providing three dimensional routing of signals and power between the layers of the substrate and further including two like sets of multilevel cavities formed therein, one set for each said T/R channel, arranged side by side and in which one or more active circuit components are respectively located; a heat sink plate bonded to the underside surface of the substrate and also covering an area including the two sets of cavities, said active circuit components being in direct contact with said heat sink plate and which thereby provides a thermal interface to an external heat exchanger; a unitary RF connector assembly including a plurality of discrete signal connectors located at one end of the substrate for independently coupling RF signals to and from said T/R channels; a power and control interface at the opposite end of the substrate for coupling DC power and operational control signals to said active circuit components located on the substrate.
73. An active aperture according to claim 72 and wherein each T/R module additionally includes: a metallized ring frame member bonded to the top of said substrate, said ring frame member bordering a major portion of the outer periphery of the substrate as well as encircling the two sets of cavities; a metallized cover member bonded to said ring frame member and covering an area including the two sets of cavities.
74. An antenna system according to claim 73 wherein said cover member includes a generally flat outer surface and wherein said heat sink plate includes generally flat inner and outer surfaces and wherein said active circuit components are located on said flat inner surface of the heat sink plate.
75. 7An active aperture according to claim 72, and additionally including, energy storage means located off of and at the opposite end of the substrate for supplying supplementary DC power to said active circuit components located on the substrate.
76. An active aperture according to claim 75 wherein said energy storage means comprise capacitive means.
77. An active aperture according to claim 76 wherein said capacitive means comprises a bank of electrical capacitors.
78. An active aperture according to claim 75 wherein capacitive energy storage means includes a plurality of capacitors located in a support housing attached to said substrate.
79. An active aperture according to claim 72 wherein each set of cavities includes three multi-level cavities having intermediate levels for providing external wire connections to the respective active circuit components located in the cavities and for mounting passive circuit components thereon.
80 An active aperture according to claim 79 wherein each set of three cavities are mutually aligned along a side edge of the substrate and wherein a first cavity of each said set includes therein a first active circuit component implementing an RF preamplifier in a transmit mode and post amplifier in a receive mode, a signal attenuator, a switch and an RF driver amplifier and a second active circuit component implementing another RF switch and a phase shifter, wherein a second cavity of each said set includes therein an active circuit component implementing a low noise amplifier, and wherein a third cavity of each said set includes an active circuit component implementing an RF output power amplifier.
81. 7An active aperture according to claim 80 and additionally including a pair of non-cavity regions at said opposite end of said two sets of cavities for locating thereat a respective active circuit component implementing module controllers for the two T/R channels.
82. An active aperture according to claim 81 and further including a non-cavity region between said two sets of cavities and said pair of non-cavity regions for locating thereat active circuit components for implementing a gate regulator, a DC power controller, a power switch which are commonly utilized by both said T/R channels.
83. An active aperture according to claim 72 and wherein said connector assembly comprises a first pair of RF input and output connectors for one of said two T/R channels, a second pair of RF input and output connectors for the other of said T/R channels, an RF receive manifold connector for both said T/R channels, and an RF transmit manifold connector for both said T/R channels, and wherein said connectors comprise blind mate press-on connectors for facilitating relatively easy connection to an antenna array, and wherein all of said connectors are mutually aligned and located in a common shroud.
84. An active aperture according to claim 72 wherein all of said plurality of ceramic HTCC layers includes at least one set of layers for providing at least one level of RF signal routing in the substrate and at least one layer for providing at least one level of DC power and control signal routing in the substrate.
85. An antenna system according to claim 84 wherein one set of said two sets of layers providing RF signal routing couples RF signals between predetermined RF input and output connectors of said connector assembly and predetermined active circuit components of said T/R channels wherein the other set of said two sets of layers include a first stripline RF signal coupler acting as a signal combiner and a second stripline RF signal coupler acting as a signal splitter formed between two adjacent layers of said other set of layers for respectively coupling RF signals between said receive manifold connector and said transmit manifold connector and predetermined active components of said T/R channels.
PCT/US1999/021745 1998-09-23 1999-09-23 A dual channel microwave transmit/receive module for an active aperture of a radar system WO2000022451A2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP2000576296A JP2002527971A (en) 1998-09-23 1999-09-23 Dual channel microwave transmit / receive module for active aperture of radar system
AT99968836T ATE258313T1 (en) 1998-09-23 1999-09-23 TWO-CHANNEL MICROWAVE TRANSMIT/RECEIVE MODULE FOR ACTIVE APPARATUS OF A RADAR SYSTEM
CA002344400A CA2344400A1 (en) 1998-09-23 1999-09-23 A dual channel microwave transmit/receive module for an active aperture of a radar system
DE69914354T DE69914354T2 (en) 1998-09-23 1999-09-23 Two-channel microwave transmitter-receiver module for an active aperture of a radar system
AU27052/00A AU2705200A (en) 1998-09-23 1999-09-23 A dual channel microwave transmit/receive module for an active aperture of a radar system
EP99968836A EP1125144B1 (en) 1998-09-23 1999-09-23 A dual channel microwave transmit/receive module for an active aperture of a radar system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/158,832 1998-09-23
US09/158,829 US6114986A (en) 1998-03-04 1998-09-23 Dual channel microwave transmit/receive module for an active aperture of a radar system

Publications (3)

Publication Number Publication Date
WO2000022451A2 true WO2000022451A2 (en) 2000-04-20
WO2000022451A3 WO2000022451A3 (en) 2000-07-27
WO2000022451A9 WO2000022451A9 (en) 2000-09-14

Family

ID=22569898

Family Applications (2)

Application Number Title Priority Date Filing Date
PCT/US1999/021745 WO2000022451A2 (en) 1998-09-23 1999-09-23 A dual channel microwave transmit/receive module for an active aperture of a radar system
PCT/US1999/022016 WO2000021159A2 (en) 1998-09-23 1999-09-23 Transmit/receive module having multiple transmit/receive paths with shared circuitry

Family Applications After (1)

Application Number Title Priority Date Filing Date
PCT/US1999/022016 WO2000021159A2 (en) 1998-09-23 1999-09-23 Transmit/receive module having multiple transmit/receive paths with shared circuitry

Country Status (9)

Country Link
US (4) US6114986A (en)
EP (2) EP1110276A2 (en)
JP (2) JP2002527971A (en)
KR (2) KR100758554B1 (en)
AT (1) ATE258313T1 (en)
AU (2) AU2705200A (en)
CA (2) CA2344427A1 (en)
DE (1) DE69914354T2 (en)
WO (2) WO2000022451A2 (en)

Families Citing this family (100)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2368213B (en) * 1997-11-03 2002-12-31 British Aerospace A non-linear dispersive pulse generator
GB2435744B (en) * 1997-11-07 2008-02-06 British Aerospace A non-linear dispersive transmission line assembly
US6114986A (en) * 1998-03-04 2000-09-05 Northrop Grumman Corporation Dual channel microwave transmit/receive module for an active aperture of a radar system
US6292133B1 (en) * 1999-07-26 2001-09-18 Harris Corporation Array antenna with selectable scan angles
DE60127662T2 (en) * 2000-04-07 2007-12-27 The Chief Controller, Research And Development, Defence Research And Development Organisation Of Ministry Of Defence TRANSMITTER / RECEIVER MODULE FOR ACTIVE PHASE ARRAYANTENNE
AU2001284984A1 (en) * 2000-08-16 2002-02-25 Raytheon Company Highly integrated single substrate mmw multi-beam sensor
US6577269B2 (en) 2000-08-16 2003-06-10 Raytheon Company Radar detection method and apparatus
JP5063851B2 (en) 2000-08-16 2012-10-31 ヴァレオ・レイダー・システムズ・インコーポレーテッド Proximity object detection system
JP2004506906A (en) 2000-08-16 2004-03-04 レイセオン・カンパニー Automotive radar system and method
EP1310018B1 (en) 2000-08-16 2018-07-25 Valeo Radar Systems, Inc. Switched beam antenna architecture
US6462410B1 (en) * 2000-08-17 2002-10-08 Sun Microsystems Inc Integrated circuit component temperature gradient reducer
US6675094B2 (en) 2000-09-08 2004-01-06 Raytheon Company Path prediction system and method
US6759743B2 (en) * 2000-09-11 2004-07-06 Xytrans, Inc. Thick film millimeter wave transceiver module
US6573863B2 (en) * 2000-12-12 2003-06-03 Harris Corporation Phased array antenna system utilizing highly efficient pipelined processing and related methods
US6708100B2 (en) 2001-03-14 2004-03-16 Raytheon Company Safe distance algorithm for adaptive cruise control
JP3612031B2 (en) * 2001-03-29 2005-01-19 Tdk株式会社 High frequency module
US6707684B1 (en) 2001-04-02 2004-03-16 Advanced Micro Devices, Inc. Method and apparatus for direct connection between two integrated circuits via a connector
US6627992B2 (en) * 2001-05-21 2003-09-30 Xytrans, Inc. Millimeter wave (MMW) transceiver module with transmitter, receiver and local oscillator frequency multiplier surface mounted chip set
GB0112454D0 (en) * 2001-05-23 2001-07-11 Astrium Ltd A module
US6646600B2 (en) * 2001-11-09 2003-11-11 Harris Corporation Phased array antenna with controllable amplifier bias adjustment and related methods
JP3964873B2 (en) * 2001-11-09 2007-08-22 株式会社日立製作所 In-vehicle millimeter wave radar system
US6841981B2 (en) * 2002-04-09 2005-01-11 Mstar Semiconductor, Inc. Radio frequency data communication device in CMOS process
US6611227B1 (en) 2002-08-08 2003-08-26 Raytheon Company Automotive side object detection sensor blockage detection system and related techniques
WO2004015764A2 (en) * 2002-08-08 2004-02-19 Leedy Glenn J Vertical system integration
US6611430B1 (en) 2002-09-04 2003-08-26 Northrop Grumman Corporation Miniature self-locking, spring action, microwave module retainer
DE10252091A1 (en) * 2002-11-08 2004-05-19 Siemens Ag Multi-static sensor arrangement for object distance measurement, e.g. for vehicle parking, has pulse generators receiving clock signals via common data bus to produce deterministic HF oscillator signal phase relationship
JP2004297486A (en) * 2003-03-27 2004-10-21 Sharp Corp Multilayer substrate for low-noise blocking down converter
DE10340438B4 (en) * 2003-09-02 2005-08-04 Epcos Ag Transmitter module with improved heat dissipation
EP1673851A4 (en) * 2003-10-17 2011-03-16 Powercast Corp Method and apparatus for a wireless power supply
US7416630B2 (en) * 2003-11-24 2008-08-26 Northrop Grumman Corporation Fabrication of LTCC T/R modules with multiple cavities and an integrated ceramic ring frame
US7240424B2 (en) * 2004-04-29 2007-07-10 Northrop Grumman Corporation Method of laminating low temperature co-fired ceramic (LTCC) Material
US6979239B1 (en) 2004-06-30 2005-12-27 Northrop Grumman Corporation Plating of brazed RF connectors for T/R modules
US7134391B2 (en) * 2004-07-22 2006-11-14 Northrop Grumman Corporation Apparatus and method for side printing on low temperature co-fired ceramic (LTCC) substrates
US7978173B2 (en) * 2005-01-14 2011-07-12 Avago Technologies Ecbu Ip (Singapore) Pte. Ltd. Pointing device including a moveable puck with mechanical detents
US7391382B1 (en) * 2005-04-08 2008-06-24 Raytheon Company Transmit/receive module and method of forming same
US7511664B1 (en) 2005-04-08 2009-03-31 Raytheon Company Subassembly for an active electronically scanned array
US7456789B1 (en) 2005-04-08 2008-11-25 Raytheon Company Integrated subarray structure
CN101283449B (en) * 2005-07-01 2014-08-20 维税-希力康克斯公司 Complete power management system implemented in a single surface mount package
US7545322B2 (en) * 2005-09-20 2009-06-09 Raytheon Company Antenna transceiver system
US9713258B2 (en) * 2006-04-27 2017-07-18 International Business Machines Corporation Integrated circuit chip packaging
US8757246B2 (en) * 2006-06-06 2014-06-24 Raytheon Company Heat sink and method of making same
US7961470B2 (en) * 2006-07-19 2011-06-14 Infineon Technologies Ag Power amplifier
US7796714B2 (en) * 2006-08-02 2010-09-14 Powerwave Cognition, Inc. Multiple signal receiving
JP4286855B2 (en) * 2006-09-07 2009-07-01 株式会社日立製作所 Radar equipment
US9172145B2 (en) 2006-09-21 2015-10-27 Raytheon Company Transmit/receive daughter card with integral circulator
US9019166B2 (en) 2009-06-15 2015-04-28 Raytheon Company Active electronically scanned array (AESA) card
US7671696B1 (en) 2006-09-21 2010-03-02 Raytheon Company Radio frequency interconnect circuits and techniques
US7573420B2 (en) * 2007-05-14 2009-08-11 Infineon Technologies Ag RF front-end for a radar system
US7844253B2 (en) * 2006-10-19 2010-11-30 Future Dial Inc. Method and apparatus for using an electromagnetically shielded enclosure for exchanging secure data
US8095088B2 (en) 2007-05-17 2012-01-10 Harris Stratex Networks Operating Corporation Compact wide dynamic range transmitter for point to point radio
US8395256B2 (en) * 2007-02-02 2013-03-12 Harris Stratex Networks Operating Corporation Packaging for low-cost, high-performance microwave and millimeter wave modules
US8275071B2 (en) 2007-05-17 2012-09-25 Harris Stratex Networks Operating Corporation Compact dual receiver architecture for point to point radio
US7782765B2 (en) 2007-01-22 2010-08-24 Harris Stratex Networks Operating Corporation Distributed protection switching architecture for point-to-point microwave radio systems
US7532163B2 (en) * 2007-02-13 2009-05-12 Raytheon Company Conformal electronically scanned phased array antenna and communication system for helmets and other platforms
US7548424B2 (en) * 2007-03-12 2009-06-16 Raytheon Company Distributed transmit/receive integrated microwave module chip level cooling system
US7570209B2 (en) * 2007-04-25 2009-08-04 The Boeing Company Antenna system including a power management and control system
US20080278370A1 (en) * 2007-05-09 2008-11-13 Rudolf Lachner Rf-frontend for a radar system
US7728771B2 (en) * 2007-07-03 2010-06-01 Northrop Grumman Systems Corporation Dual band quadpack transmit/receive module
GB0716116D0 (en) * 2007-08-17 2007-09-26 Selex Sensors & Airborne Sys Antenna
KR101191293B1 (en) 2008-03-31 2012-10-16 발레오 레이더 시스템즈, 인크. Automotive radar sensor blockage detection apparatus and method
US8022861B2 (en) 2008-04-04 2011-09-20 Toyota Motor Engineering & Manufacturing North America, Inc. Dual-band antenna array and RF front-end for mm-wave imager and radar
US7733265B2 (en) * 2008-04-04 2010-06-08 Toyota Motor Engineering & Manufacturing North America, Inc. Three dimensional integrated automotive radars and methods of manufacturing the same
US7830301B2 (en) * 2008-04-04 2010-11-09 Toyota Motor Engineering & Manufacturing North America, Inc. Dual-band antenna array and RF front-end for automotive radars
FR2936610B1 (en) * 2008-09-30 2011-11-25 Thales Sa MODULE FOR TRANSMITTING AND RECEIVING X-BAND X-FREQUENCY SIGNALS ON MULTI-LAYER CIRCUIT AND ACTIVE ANTENNA
US7990237B2 (en) * 2009-01-16 2011-08-02 Toyota Motor Engineering & Manufacturing North America, Inc. System and method for improving performance of coplanar waveguide bends at mm-wave frequencies
US7965235B2 (en) * 2009-02-24 2011-06-21 Raytheon Company Multi-channel thinned TR module architecture
US7876263B2 (en) * 2009-02-24 2011-01-25 Raytheon Company Asymmetrically thinned active array TR module and antenna architecture
US7859835B2 (en) 2009-03-24 2010-12-28 Allegro Microsystems, Inc. Method and apparatus for thermal management of a radio frequency system
RU2525747C2 (en) * 2009-04-01 2014-08-20 Конинклейке Филипс Электроникс Н.В. Noise matching in coupled antenna arrays
US8102084B2 (en) 2009-09-18 2012-01-24 Ubidyne, Inc. Bus bar power distribution for an antenna embedded radio system
GB2473663B (en) * 2009-09-21 2016-11-23 Aveillant Ltd Radar Receiver
US8537552B2 (en) 2009-09-25 2013-09-17 Raytheon Company Heat sink interface having three-dimensional tolerance compensation
US8508943B2 (en) 2009-10-16 2013-08-13 Raytheon Company Cooling active circuits
US20110159824A1 (en) * 2009-12-31 2011-06-30 Peter Kenington Active antenna array for a mobile communications network employing a first conductive layer and a second conductive layer
US8427371B2 (en) 2010-04-09 2013-04-23 Raytheon Company RF feed network for modular active aperture electronically steered arrays
US8786496B2 (en) 2010-07-28 2014-07-22 Toyota Motor Engineering & Manufacturing North America, Inc. Three-dimensional array antenna on a substrate with enhanced backlobe suppression for mm-wave automotive applications
JP5736716B2 (en) * 2010-10-15 2015-06-17 富士通株式会社 Electronic device, manufacturing method thereof, and transmitting / receiving device
US8810448B1 (en) 2010-11-18 2014-08-19 Raytheon Company Modular architecture for scalable phased array radars
US8355255B2 (en) 2010-12-22 2013-01-15 Raytheon Company Cooling of coplanar active circuits
US9182485B1 (en) * 2011-05-24 2015-11-10 Garmin International, Inc. Transmit/receive module for electronically steered weather radar
US9124361B2 (en) 2011-10-06 2015-09-01 Raytheon Company Scalable, analog monopulse network
US9276332B2 (en) 2013-03-15 2016-03-01 Fct, Us L.L.C. High-temperature RF connector
US9871296B2 (en) 2013-06-25 2018-01-16 Huawei Technologies Co., Ltd. Mixed structure dual-band dual-beam three-column phased array antenna
WO2016029222A1 (en) * 2014-08-22 2016-02-25 Google Inc. Systems and methods for enabling radio-frequency communication of a modular mobile electronic device
US9402301B2 (en) * 2014-12-10 2016-07-26 Raytheon Company Vertical radio frequency module
CN106020018B (en) * 2016-05-17 2019-01-04 中国电子科技集团公司第四十一研究所 TR component programmable state controller and working method based on USB
US10833408B2 (en) 2017-07-07 2020-11-10 Rockwell Collins, Inc. Electronically scanned array
US10910709B1 (en) * 2018-01-22 2021-02-02 Rockwell Collins, Inc. Control architecture for electronically scanned array
CN108768438B (en) * 2018-08-21 2023-10-10 无锡华测电子系统有限公司 Solid 64-channel receiving and transmitting assembly
CN109586757B (en) * 2018-12-14 2020-08-14 北京遥测技术研究所 Transmit-receive duplex drive amplification power division network
US11382224B2 (en) * 2019-02-26 2022-07-05 Pa&E, Hermetic Solutions Group, Llc Hermetically sealed electronic packages with electrically powered multi-pin electrical feedthroughs
IL268104B2 (en) * 2019-07-16 2024-01-01 Elta Systems Ltd Compact array antenna system
CN110596647A (en) * 2019-10-17 2019-12-20 成都锐芯盛通电子科技有限公司 High integration TR module based on SIP encapsulation
US20220075022A1 (en) * 2020-02-04 2022-03-10 Macom Technology Solutions Holdings, Inc. Configurable radar tile architecture
CN111258259B (en) * 2020-04-27 2020-07-28 浙江航芯源集成电路科技有限公司 Multi-channel high-integration surface-mounted TR component control chip
TWM610606U (en) * 2020-04-27 2021-04-21 訊鼎電子股份有限公司 Signal Configurator
WO2022051986A1 (en) * 2020-09-10 2022-03-17 罗森伯格技术有限公司 Double-beam feed network and hybrid network antenna with double-beam feed network
CN112564730B (en) * 2020-11-13 2022-08-12 北京遥测技术研究所 High-reliability multi-output power TR assembly with flexible design
CN113098551B (en) * 2021-04-27 2022-01-04 电子科技大学 HTCC three-dimensional receiving and transmitting assembly
CN113093117B (en) * 2021-06-03 2021-09-07 成都雷电微晶科技有限公司 Millimeter wave single-channel control TR component

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4967201A (en) * 1987-10-22 1990-10-30 Westinghouse Electric Corp. Multi-layer single substrate microwave transmit/receive module
US5276455A (en) * 1991-05-24 1994-01-04 The Boeing Company Packaging architecture for phased arrays
US5431582A (en) * 1994-03-28 1995-07-11 Raytheon Company Module retention apparatus
US5745076A (en) * 1996-09-05 1998-04-28 Northrop Grumman Corporation Transmit/receive module for planar active apertures

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3818386A (en) * 1967-04-03 1974-06-18 Texas Instruments Inc Solid-state modular microwave system
US3750175A (en) * 1967-12-14 1973-07-31 Texas Instruments Inc Modular electronics communication system
US3643075A (en) * 1970-12-02 1972-02-15 Texas Instruments Inc Digital simulation
US3899720A (en) * 1973-09-14 1975-08-12 Westinghouse Electric Corp Package for microwave integrated circuits
US4823136A (en) * 1987-02-11 1989-04-18 Westinghouse Electric Corp. Transmit-receive means for phased-array active antenna system using rf redundancy
US4998181A (en) * 1987-12-15 1991-03-05 Texas Instruments Incorporated Coldplate for cooling electronic equipment
US4870421A (en) * 1987-12-28 1989-09-26 General Electric Company Regulating switch for transmitting modules in a phased array radar
US4806937A (en) * 1987-12-31 1989-02-21 General Electric Company Power distribution system for a phased array radar
US5412414A (en) * 1988-04-08 1995-05-02 Martin Marietta Corporation Self monitoring/calibrating phased array radar and an interchangeable, adjustable transmit/receive sub-assembly
US5214498A (en) * 1990-02-26 1993-05-25 Raytheon Company MMIC package and connector
US5155492A (en) * 1991-05-29 1992-10-13 Westinghouse Electric Corp. Dual mode active aperture
US5225841A (en) * 1991-06-27 1993-07-06 Hughes Aircraft Company Glittering array for radar pulse shaping
US5140333A (en) * 1991-08-23 1992-08-18 Westinghouse Electric Corp. System and method for operating transmit/receive modules of active aperture phased array antennas
JP2560001Y2 (en) * 1991-09-04 1998-01-21 三菱電機株式会社 Transmission / reception module
US5264860A (en) * 1991-10-28 1993-11-23 Hughes Aircraft Company Metal flared radiator with separate isolated transmit and receive ports
NL9101979A (en) * 1991-11-27 1993-06-16 Hollandse Signaalapparaten Bv PHASED ARRAY ANTENNA MODULE.
US5353033A (en) * 1993-04-15 1994-10-04 Hughes Aircraft Company Optoelectronic phased array with digital transmit signal interface
US5442364A (en) * 1993-07-22 1995-08-15 The United States Of America As Represented By The Secretary Of The Navy Alignment and beam spreading for ground radial airborne radar
US5382175A (en) * 1993-07-28 1995-01-17 E-Systems, Inc. Thermal core wedge clamp
US5386339A (en) * 1993-07-29 1995-01-31 Hughes Aircraft Company Monolithic microelectronic circuit package including low-temperature-cofired-ceramic (LTCC) tape dielectric structure and in-situ heat sink
US5457607A (en) * 1994-03-28 1995-10-10 Raytheon Company Unified module housing
US5539415A (en) * 1994-09-15 1996-07-23 Space Systems/Loral, Inc. Antenna feed and beamforming network
US5559519A (en) * 1995-05-04 1996-09-24 Northrop Grumman Corporation Method and system for the sequential adaptive deterministic calibration of active phased arrays
US5854610A (en) * 1997-11-13 1998-12-29 Northrop Grumman Corporation Radar electronic scan array employing ferrite phase shifters
US6114986A (en) * 1998-03-04 2000-09-05 Northrop Grumman Corporation Dual channel microwave transmit/receive module for an active aperture of a radar system
US5861845A (en) * 1998-05-19 1999-01-19 Hughes Electronics Corporation Wideband phased array antennas and methods
US6005531A (en) * 1998-09-23 1999-12-21 Northrop Grumman Corporation Antenna assembly including dual channel microwave transmit/receive modules

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4967201A (en) * 1987-10-22 1990-10-30 Westinghouse Electric Corp. Multi-layer single substrate microwave transmit/receive module
US5276455A (en) * 1991-05-24 1994-01-04 The Boeing Company Packaging architecture for phased arrays
US5431582A (en) * 1994-03-28 1995-07-11 Raytheon Company Module retention apparatus
US5745076A (en) * 1996-09-05 1998-04-28 Northrop Grumman Corporation Transmit/receive module for planar active apertures

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
WEIN D ET AL: "Microwave and millimeter-wave packaging and interconnection methods for single and multiple chip modules" 15TH ANNUAL GAAS IC SYMPOSIUM TECHNICAL DIGEST 1993, 15TH ANNUAL GAAS IC SYMPOSIUM, SAN JOSE, CA, USA, 10-13 OCT. 1993, pages 333-336, XP002137405 Oct. 1993, New York, NY, USA, IEEE, USA ISBN: 0-7803-1393-3 *

Also Published As

Publication number Publication date
AU2705200A (en) 2000-05-01
KR20010079871A (en) 2001-08-22
CA2344427A1 (en) 2000-04-13
JP2002527724A (en) 2002-08-27
US6097335A (en) 2000-08-01
US6278400B1 (en) 2001-08-21
EP1125144A2 (en) 2001-08-22
KR100758554B1 (en) 2007-09-13
DE69914354D1 (en) 2004-02-26
DE69914354T2 (en) 2004-11-11
WO2000021159A2 (en) 2000-04-13
WO2000021159A3 (en) 2000-07-27
US6094161A (en) 2000-07-25
KR100707910B1 (en) 2007-04-16
WO2000022451A9 (en) 2000-09-14
WO2000022451A3 (en) 2000-07-27
JP2002527971A (en) 2002-08-27
EP1125144B1 (en) 2004-01-21
KR20010079872A (en) 2001-08-22
ATE258313T1 (en) 2004-02-15
CA2344400A1 (en) 2000-04-20
US6114986A (en) 2000-09-05
EP1110276A2 (en) 2001-06-27
AU2472100A (en) 2000-04-26

Similar Documents

Publication Publication Date Title
EP1125144B1 (en) A dual channel microwave transmit/receive module for an active aperture of a radar system
EP1590859B1 (en) Low profile active electronically scanned antenna (aesa) for ka-band radar systems
US8643548B2 (en) Dual beam dual selectable polarization antenna
EP1921709B1 (en) Compact, dual-beam, phased array antenna architecture
US6580402B2 (en) Antenna integrated ceramic chip carrier for a phased array antenna
US6130640A (en) Radar module and MMIC package for use in such radar module
EP3032651A1 (en) Switchable transmit and receive phased array antenna
US7728771B2 (en) Dual band quadpack transmit/receive module
Axness et al. Shared aperture technology development
US7289078B2 (en) Millimeter wave antenna
US6034633A (en) Transmit/receive module having multiple transmit/receive paths with shared circuitry
US11462837B2 (en) Array antenna
US5262794A (en) Monolithic gallium arsenide phased array using integrated gold post interconnects
CN116526138A (en) Phased array antenna with transmit-receive filtering design
CN117638495A (en) Phased array antenna subarray with high isolation

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A2

Designated state(s): AU CA JP KR

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
AK Designated states

Kind code of ref document: A3

Designated state(s): AU CA JP KR

AL Designated countries for regional patents

Kind code of ref document: A3

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE

AK Designated states

Kind code of ref document: C2

Designated state(s): AU CA JP KR

AL Designated countries for regional patents

Kind code of ref document: C2

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE

COP Corrected version of pamphlet

Free format text: PAGES 1/14-14/14, DRAWINGS, REPLACED BY NEW PAGES 1/26-26/26

WWE Wipo information: entry into national phase

Ref document number: 27052/00

Country of ref document: AU

ENP Entry into the national phase

Ref document number: 2344400

Country of ref document: CA

Kind code of ref document: A

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 1020017003570

Country of ref document: KR

ENP Entry into the national phase

Ref document number: 2000 576296

Country of ref document: JP

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 1999968836

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: 1999968836

Country of ref document: EP

Ref document number: 1020017003570

Country of ref document: KR

WWG Wipo information: grant in national office

Ref document number: 1999968836

Country of ref document: EP

WWR Wipo information: refused in national office

Ref document number: 1020017003570

Country of ref document: KR